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Paper Citation Record · LEDGER

Lift augmentation by incorporating bend twist coupled composites in flapping wing

As of 8 August 2026, this Paper Citation Record lists 69 of 69 outbound references and 0 inbound Pith citation observations for arXiv:2505.23372.

A citation records a reference. It does not transfer a finding from one paper to another.

pith.paper-citation-record.v1
2505.23372 v1

Coverage vector

measured 69 of 69 reference resolution

Typed states for the displayed outbound observations.

Source: paper_references, paper_reference_links, observed 2026-08-07T12:51:50.084806Z

measured 69 of 69 standing notices

One-hop event checks from named stored sources.

Source: scholarly_work_events, retraction_status_cache, observed 2026-08-07T06:34:17.273281+00:00

measured 0 of 0 inbound itemization

Pith citing papers itemized under the disclosed page cap.

Source: paper_references, paper_reference_links

measured 0 of 1 external citation measurements

A source-named dated measurement, never combined with another source.

Source: cited_works

Reference resolution

69 of 69 outbound references displayed

  • verified exact8
  • verified fuzzy53
  • unresolved6
  • parse uncertain0
  • malformed identifier0
  • metadata mismatch2

External citation measurements

No source-named external measurement is stored.

Outbound references

Observation 94081338-5cb2-4769-836d-0987aa7793d0 · outbound

This paper cites Two dimensional mechanism for insect hovering,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Two dimensional mechanism for insect hovering,

Reference 1

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verified fuzzy
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Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

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Observation fbd90933-f8a0-43d0-8999-e9024d648bd8 · outbound

This paper cites Bumblebee flight in heavy turbulence,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Bumblebee flight in heavy turbulence,

Reference 2

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Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

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Observation 6209d268-c7c2-430d-9984-d0485a1d47f2 · outbound

This paper cites Flapping wing flight can save aerodynamic power compared to steady flight,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Flapping wing flight can save aerodynamic power compared to steady flight,

Reference 3

Resolution
verified fuzzy
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Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

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Observation ab483284-6b87-4034-8b82-711953c984e2 · outbound

This paper cites Collective flow enhancement by tandem flapping wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Collective flow enhancement by tandem flapping wings,

Reference 4

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verified fuzzy
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Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

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Observation 5c5430d6-5a82-4df6-93ac-839aba122c7c · outbound

This paper cites an unresolved cited work.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Unresolved cited work

Reference 5

Resolution
unresolved
raw_fallback, observed 2026-08-07T12:52:37.880462Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

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Observation aafdfea6-7ac4-4cf0-b65b-a968cdd58dd6 · outbound

This paper cites Aerodynamic efficiency explains flapping strategies used by birds,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Aerodynamic efficiency explains flapping strategies used by birds,

Reference 6

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:37.680241Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

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Observation cb2c7858-09bf-4e36-ac8e-32a85bf6a5fc · outbound

This paper cites Wing kinematics of avian flight across speeds,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Wing kinematics of avian flight across speeds,

Reference 7

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:37.446012Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

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Observation 62caafba-c800-4e27-95d2-04d7746c067e · outbound

This paper cites Aerodynamic performance and flow mechanism of 3D flapping wing using discrete vo rtex method,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Aerodynamic performance and flow mechanism of 3D flapping wing using discrete vo rtex method,

Reference 8

Resolution
metadata mismatch
raw_fallback, observed 2026-08-07T12:51:52.519972Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:43.200591Z digest=sha256:dbe04c424078d068084667164d42d6b544c25da68179155c88de76d50b58a20b

Observation 0f636f43-7f44-4746-a986-feb091775e62 · outbound

This paper cites Numerical simulations of bio -inspired approaches to enhance underwater swimming efficiency ,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Numerical simulations of bio -inspired approaches to enhance underwater swimming efficiency ,

Reference 9

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unresolved
no resolver link, observed 2026-08-07T12:51:43.392036Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

source=pdf_text observed=2026-08-07T12:51:43.392036Z digest=sha256:3273ea5247066db870bd83dd15317e8fad7794ff49bbc9bee30b354efa8224f8

Observation 88ac062e-409d-424f-a847-ad8350ac25af · outbound

This paper cites Vortex wake and flight kinematics of a swift in cruising flight in a wind tunnel,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Vortex wake and flight kinematics of a swift in cruising flight in a wind tunnel,

Reference 10

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:37.139978Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:43.574703Z digest=sha256:4f690dc75f46f9ade10e55349890967ddd6d0e33f979c0b19553673fcf154886

Observation 29672e26-fe31-4544-905c-fd4d9b101889 · outbound

This paper cites Effects of flexibility on the aerodynamic performance of flapping wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Effects of flexibility on the aerodynamic performance of flapping wings,

Reference 11

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:36.815750Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:43.703182Z digest=sha256:e7c7ff9b7fb9a29e75b85597d61ffe04fd165a03558c391eaab6c94cfdaafe70

Observation c2370164-99a4-4e3b-ab5e-0ceba6760733 · outbound

This paper cites Optimization ‐ based study of bend –twist coupled rotor blades for passive and integrated passive/active load alleviation,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Optimization ‐ based study of bend –twist coupled rotor blades for passive and integrated passive/active load alleviation,

Reference 12

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:01.651615Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:43.814060Z digest=sha256:a86562a95eab413ceaf31a4089255ea1a892455029453d2002fd7a8f80539563

Observation 6e673fb0-4926-438b-a692-09aa8a37159b · outbound

This paper cites Optimal Design of Wind Turbine Blades with Bend -Twist Couplings Effects,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Optimal Design of Wind Turbine Blades with Bend -Twist Couplings Effects,

Reference 13

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:01.527024Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:43.917241Z digest=sha256:de7d501f26a18a7bae91b8bd38c6f27de058f4e7369921cbec933f53962738d2

Observation 8493bcd7-a17b-4e94-9828-f0678b1bf809 · outbound

This paper cites Numerical investigation of an insect -scale flexible wing with a small amplitude flapping kinematics,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Numerical investigation of an insect -scale flexible wing with a small amplitude flapping kinematics,

Reference 14

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verified fuzzy
raw_fallback, observed 2026-08-07T12:52:01.378100Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:44.022376Z digest=sha256:0e699417aa8ff66c8bab4cb88b235eda34e29c77be210c49f834c0b9798b9f02

Observation 301f7683-db06-41a4-b19e-e2f538b33805 · outbound

This paper cites Aerodynamic technologies to improve aircraft performance,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Aerodynamic technologies to improve aircraft performance,

Reference 15

Resolution
verified fuzzy
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Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

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Observation e6912c8c-53b9-458e-bcb3-9cf08f024c9d · outbound

This paper cites On the role of vortical structures in aerodynamic performance of a hovering mosquito,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing On the role of vortical structures in aerodynamic performance of a hovering mosquito,

Reference 16

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:01.090704Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:44.253332Z digest=sha256:3f7b426db5629442b025e3da50463c85164ae8a50e4fafcba82a7384b97ceb0f

Observation 4d95ab42-266a-46c5-85af-5cd498462161 · outbound

This paper cites Aerodynamic interaction of bristled wing pairs in fling,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Aerodynamic interaction of bristled wing pairs in fling,

Reference 17

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verified fuzzy
raw_fallback, observed 2026-08-07T12:52:00.904261Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

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Observation 38df10bc-a0d0-4add-91d3-846c58e54a32 · outbound

This paper cites Aerodynamic performance of a free - flying dragonfly—A span-resolved investigation,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Aerodynamic performance of a free - flying dragonfly—A span-resolved investigation,

Reference 18

Resolution
verified fuzzy
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Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

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Observation f80dfd98-a1d9-4b3c-b681-d8ffde2a1553 · outbound

This paper cites The spatial -temporal effects of wing 19 flexibility on aerodynamic performance of the flapping wing,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing The spatial -temporal effects of wing 19 flexibility on aerodynamic performance of the flapping wing,

Reference 19

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:00.485451Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:44.546123Z digest=sha256:ba66a8d626331a1989995a09d7f7f5c4aa18de6d4a8ec90d2b021923bafd1970

Observation 9e45bfec-e14d-42e5-8be3-50a4423574a9 · outbound

This paper cites Extension -twist coupling optimization in composite rotor blades,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Extension -twist coupling optimization in composite rotor blades,

Reference 20

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:00.332982Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

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Observation 7536b3c3-88cb-45c6-bcf0-5c679497010f · outbound

This paper cites Optimization of extension -twist coupled composite blades for high -speed rotorcraft,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Optimization of extension -twist coupled composite blades for high -speed rotorcraft,

Reference 21

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:52:00.166243Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

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Observation 88a5f178-816b-47a9-9a3a-0e96c7afb107 · outbound

This paper cites Non -linear aeroelastic prediction for aircraft applications,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Non -linear aeroelastic prediction for aircraft applications,

Reference 22

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verified fuzzy
raw_fallback, observed 2026-08-07T12:51:59.999545Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

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Observation 2646af20-8520-4aec-b543-cad2ee70bba6 · outbound

This paper cites Advances in biomedical fluid –structure interaction: Methodologies and applications from an interfacing perspective,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Advances in biomedical fluid –structure interaction: Methodologies and applications from an interfacing perspective,

Reference 23

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:59.791408Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:44.999555Z digest=sha256:1b4f51fd91b587f99d492209d89ac9af8609d07e6f97aee92f414197c0db4a78

Observation c8ab408b-16cf-4464-98e2-cdc7e2e136e9 · outbound

This paper cites Numerical investigation of structural geometric nonlinearity effect in high -aspect-ratio wing using CFD/CSD coupled approach,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Numerical investigation of structural geometric nonlinearity effect in high -aspect-ratio wing using CFD/CSD coupled approach,

Reference 24

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verified fuzzy
raw_fallback, observed 2026-08-07T12:51:59.641720Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:45.105143Z digest=sha256:e606f99dd8defd2d2cd4682a4ccd09aeaa730b99317c5bd9845bfbdba512e83c

Observation 4f38b105-d3c8-47bc-b9b1-1a9b42e846fd · outbound

This paper cites Experimental and theoretical study on aeroelastic response of high-aspect-ratio wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Experimental and theoretical study on aeroelastic response of high-aspect-ratio wings,

Reference 25

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verified fuzzy
raw_fallback, observed 2026-08-07T12:51:59.435483Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

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Observation 2c896ac4-a7eb-475c-a2e4-a7194872e9cc · outbound

This paper cites CFD -based analysis of nonlinear aeroelastic behavior of high -aspect ratio wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing CFD -based analysis of nonlinear aeroelastic behavior of high -aspect ratio wings,

Reference 26

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:59.224930Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:45.273479Z digest=sha256:23bd2d155e7054bccad654c04bc78047ae8a575f9a5b088ac04938c5e8e13af2

Observation b4b8af94-041b-4fc3-813c-0a8cfa78c65f · outbound

This paper cites Numerical investigation of nonlinear aeroelastic effects on flexible high- aspect-ratio wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Numerical investigation of nonlinear aeroelastic effects on flexible high- aspect-ratio wings,

Reference 27

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:58.923081Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:45.349571Z digest=sha256:e0149e58ab06a05c5a993ee951275446fa26e4f3375de23400f1523a318a4d8c

Observation 180f011e-38fe-4050-974f-10dab49fd730 · outbound

This paper cites Investigations on the effects of structural damping on vortex -induced vibration response of an airfoil at a high angle of attack via the aero-damping map,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Investigations on the effects of structural damping on vortex -induced vibration response of an airfoil at a high angle of attack via the aero-damping map,

Reference 28

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:58.757133Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

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Observation 6fe61089-5f67-4c1f-9bc3-6f4608a81f57 · outbound

This paper cites Fluid –structure interaction on vibrating square prisms considering interference effects,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Fluid –structure interaction on vibrating square prisms considering interference effects,

Reference 29

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:58.536704Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:45.538818Z digest=sha256:e2664df753be3da79f49a5d4dab57818942e006b65d4a54353125390bf270de3

Observation 99d8a52a-4079-403f-ad4b-de8805079c05 · outbound

This paper cites Effect of wingtip bending morphing on gust-induced aerodynamics based on fluid-structure interaction method,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Effect of wingtip bending morphing on gust-induced aerodynamics based on fluid-structure interaction method,

Reference 30

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:58.370497Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:45.647170Z digest=sha256:13633b69228a5bddfbcf01e576e606bf4e937b4e1e6aad9063ca3a9f69c726cd

Observation cef6b48c-5c82-4460-b347-7b1ad26318f5 · outbound

This paper cites Unsteady flow control mechanisms of a bio - inspired flexible flap with the fluid –structure interaction,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Unsteady flow control mechanisms of a bio - inspired flexible flap with the fluid –structure interaction,

Reference 31

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:58.152555Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:45.756847Z digest=sha256:79cdcf4270f78a95dfdc2978660d092be269c6b2c1a3d05c10b724f5e5450213

Observation 7254eedd-977c-4f3c-b217-fcfb9e60f4a3 · outbound

This paper cites Wake -induced vibration of an elastic plate submerged in the wake of tandem circular cylinders,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Wake -induced vibration of an elastic plate submerged in the wake of tandem circular cylinders,

Reference 32

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:57.969547Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:45.830889Z digest=sha256:a4ba135f7ae9e1e0456f47d8e1e0fc1383efd6f98f02fa235e02307b0a440891

Observation 46608fdb-47cd-4531-b523-f4a6494d1bfe · outbound

This paper cites Flow -induced response and wake characteristics of a flexible splitter plate attached to a circular cylinder in laminar flow,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Flow -induced response and wake characteristics of a flexible splitter plate attached to a circular cylinder in laminar flow,

Reference 33

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:57.768305Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:45.943988Z digest=sha256:2aaa0e341976d76415bfe8f8ec5b463f7da50495f9bdf395432092d4f6cd2c22

Observation 0906b812-4dec-4fc7-9643-d8a3e2ae95c4 · outbound

This paper cites Bend -Twist Coupled Carbon -Fiber Laminate Beams: Fundamental Behavior and Applications,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Bend -Twist Coupled Carbon -Fiber Laminate Beams: Fundamental Behavior and Applications,

Reference 34

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verified fuzzy
raw_fallback, observed 2026-08-07T12:51:57.558661Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:46.071660Z digest=sha256:8d5ff1fff3722590cd09be3abe6d805239d201a537767db9d4d21d0280a51a18

Observation d689c622-6e7d-4bfa-af82-6332e2011a3f · outbound

This paper cites Computationally efficient optimal design of hygrothermally stable laminate with bend –twist coupling by analytical and numerical strategy,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Computationally efficient optimal design of hygrothermally stable laminate with bend –twist coupling by analytical and numerical strategy,

Reference 35

Resolution
unresolved
no resolver link, observed 2026-08-07T12:51:46.208056Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

source=pdf_text observed=2026-08-07T12:51:46.208056Z digest=sha256:e374ce0875f0869672f5c19a74e303680f041ed78bd534322708c98368f227e4

Observation c4453fbc-84e9-4704-8cc4-43805cdd2b21 · outbound

This paper cites Effect of spanwise flexibility on flapping wing propulsion,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Effect of spanwise flexibility on flapping wing propulsion,

Reference 36

Resolution
verified exact
doi, observed 2026-08-07T12:51:51.801244Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:46.343266Z digest=sha256:f780584f71c6b33538cbffadffdd42961ce7ac5bdd28728d766e19a938f5962f

Observation 14a5425e-6ff7-4601-88de-d8e1ff5a2b33 · outbound

This paper cites High -fidelity aeroelastic computations of a flapping wing with spanwise flexibility,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing High -fidelity aeroelastic computations of a flapping wing with spanwise flexibility,

Reference 37

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:57.331414Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:46.435517Z digest=sha256:dc3a6183bb9bb000babb053c1e3d7c8f06cf9e00b7ebd78bbc2c7fbb16777d12

Observation 2f5d5225-2ba0-451f-9a43-4dd8cfd44667 · outbound

This paper cites an unresolved cited work.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Unresolved cited work

Reference 38

Resolution
unresolved
raw_fallback, observed 2026-08-07T12:51:57.136136Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:46.549775Z digest=sha256:bbabe6622cbbdbaf850933b92f38bdfb0a70e82d9ab6f9455f35de21ebc57d51

Observation 49fd7466-49ea-42a2-a54b-abd271c7bed8 · outbound

This paper cites A mixed -time-scale SGS model with fixed model-parameters for practical LES,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing A mixed -time-scale SGS model with fixed model-parameters for practical LES,

Reference 39

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:56.960614Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:46.673706Z digest=sha256:f8b8089d8487b1dd9cc91ea907ff39d188ae9e1b05b8859b86f4ee0c191adc48

Observation 142276db-d8b5-43bb-ad02-6301f9932a68 · outbound

This paper cites Modelling the effect of freestream turbulence on dynamic stall of wind turbine blades,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Modelling the effect of freestream turbulence on dynamic stall of wind turbine blades,

Reference 40

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:56.746459Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:46.778306Z digest=sha256:aab5cd78c71cb6b4da39feda99a702525d00248dff6cdba0ccf6428f4eb5c24c

Observation 35f482fc-002b-47bf-b926-885c73b0c633 · outbound

This paper cites Three - dimensional simulation for fast forward flight of a calliope hummingbird,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Three - dimensional simulation for fast forward flight of a calliope hummingbird,

Reference 41

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:56.581718Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:46.918622Z digest=sha256:0b53d513197e58c64b25e45c2a7dd54d7d07e4516fb344e8de25cc12dc21b61d

Observation 88a904c0-3124-4a36-ab26-c57aac2c9f00 · outbound

This paper cites Aerodynamics of bird flight,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Aerodynamics of bird flight,

Reference 42

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:56.400456Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:47.031605Z digest=sha256:e53633e91f87e5463bdf0dea5f017c1c78b2c44129f22c6c4d09d757bcd29a81

Observation a86a3410-f8f9-4d92-a277-7e993982f549 · outbound

This paper cites ANSYS Fluent Theory Guide, Release 18.0. Ansys,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing ANSYS Fluent Theory Guide, Release 18.0. Ansys,

Reference 43

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:56.234921Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:47.136624Z digest=sha256:d6f078c7b54610e39b7e8f99fd3e81e58e41812e7483d41dd5700d3dc634e4b0

Observation 13aa02c4-0e59-4c4d-bd43-5bd0a8251581 · outbound

This paper cites A fluid mechanicians view of wind engineering: Large eddy simulation of flow past a cubic obstacle,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing A fluid mechanicians view of wind engineering: Large eddy simulation of flow past a cubic obstacle,

Reference 44

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:56.095968Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:47.238560Z digest=sha256:9265daaf2adc752c163d420a7dd08970d6666293095f3ef3f569ec289037cd1d

Observation 8adbf2ec-d75c-4b56-a8ae-6def88980213 · outbound

This paper cites ERCOFTAC/IAHR/COST workshop on refined flow modeling,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing ERCOFTAC/IAHR/COST workshop on refined flow modeling,

Reference 45

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:55.928825Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:47.356552Z digest=sha256:8dc3d3c17d79fdea99efc44d9e1ec7aaf257137a68b11c1b562af2c65758b802

Observation 497f781a-c120-4368-9614-a8759657f933 · outbound

This paper cites Numerical simulation of flapping wing aerodynamic performance under gust wind conditions,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Numerical simulation of flapping wing aerodynamic performance under gust wind conditions,

Reference 46

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:55.744625Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:47.483388Z digest=sha256:60c5281f8a4862e3940540ff75a082b27ab11e65fc9af05282b1a6863b4647c9

Observation 218d4f29-b027-459a-8f04-8c33c8584c33 · outbound

This paper cites Numerical simulation of bending and length -varying flapping wing using discrete vortex method,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Numerical simulation of bending and length -varying flapping wing using discrete vortex method,

Reference 47

Resolution
verified exact
doi, observed 2026-08-07T12:51:51.601844Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:47.565355Z digest=sha256:e906b0b00ca11a6ad92745061653e10e288e8cc288e44a959d1ef93281767a20

Observation 116bb49b-71d0-47bc-85ef-4e0924804c11 · outbound

This paper cites Global optimization of actively morphing flapping wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Global optimization of actively morphing flapping wings,

Reference 48

Resolution
verified exact
doi, observed 2026-08-07T12:51:51.408312Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:47.674173Z digest=sha256:7e92c1f100702499da3e584ab25e7d52057f08273e17e5a1f4d3b1767137f5cf

Observation 3b7b843f-79da-45f4-8fc1-8cfbe340e901 · outbound

This paper cites Object -oriented unsteady vortex lattice method for flapping flight,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Object -oriented unsteady vortex lattice method for flapping flight,

Reference 49

Resolution
unresolved
no resolver link, observed 2026-08-07T12:51:47.803652Z

Source-reported events for the cited work

Unavailable: canonical work link unavailable.

source=pdf_text observed=2026-08-07T12:51:47.803652Z digest=sha256:e4c55a79fceac302400aa7741dd7142b05564e8a1e79242e77b5592475314dff

Observation b3af665f-5fb6-4743-993d-229b05770a15 · outbound

This paper cites Lift and Thrust Characteristics of Flapping Wing Aerial Vehicle with Pitching and Flapping Motion,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Lift and Thrust Characteristics of Flapping Wing Aerial Vehicle with Pitching and Flapping Motion,

Reference 50

Resolution
metadata mismatch
raw_fallback, observed 2026-08-07T12:51:52.112818Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:47.919310Z digest=sha256:8af1beb81ca7089cbe470eebb55b70f69f2a3a5268a4d71bf165d30e69c37b70

Observation e0e9902f-7f48-409f-a5cf-c36e59409276 · outbound

This paper cites Comparison of 2D finite element modeling assumptions with results from 3D analysis for composite skin - stiffener debonding,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Comparison of 2D finite element modeling assumptions with results from 3D analysis for composite skin - stiffener debonding,

Reference 51

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:55.523070Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:48.016309Z digest=sha256:ac8f2935e8b52e9ea40e234e2492e6df24ca4c45b317a482dc99224a360f6ed6

Observation a945eab1-1d2c-46a2-8c54-5a9915de5b9c · outbound

This paper cites Z., W., Gursul, I.: Effect of spanwise flexibility on flapping wing propulsion,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Z., W., Gursul, I.: Effect of spanwise flexibility on flapping wing propulsion,

Reference 52

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:55.330570Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:48.138642Z digest=sha256:ca3372dd72bfcd2c53b8330cf203f192ac6216bb173c5ecda4edbce253402ac3

Observation 6d19504d-452b-4b2e-b92a-51c066603d10 · outbound

This paper cites SDM 2013 student papers competition passive gust load alleviation through bend -twist coupling of composite beams on typical commercial airplane wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing SDM 2013 student papers competition passive gust load alleviation through bend -twist coupling of composite beams on typical commercial airplane wings,

Reference 53

Resolution
verified exact
doi, observed 2026-08-07T12:51:51.108968Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:48.251585Z digest=sha256:e80cce7e714568e9612f4f1920d200cdd15c58e45848d2124af9151c79e0fc28

Observation 45feb459-d8d1-47f2-b7ed-e117f560407a · outbound

This paper cites A generalized von Mises criterion for yield and fracture,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing A generalized von Mises criterion for yield and fracture,

Reference 54

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:55.141992Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:48.361587Z digest=sha256:76981345f3929c3af1d3a8f190d6f8ee501c8bab483410682e08ea4b49c0e3e7

Observation 726ff7eb-b376-4c03-8773-f85686f708a9 · outbound

This paper cites Stress Analysis of Composite Aircraft Wing using Coupled Fluid-Structural Analysis,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Stress Analysis of Composite Aircraft Wing using Coupled Fluid-Structural Analysis,

Reference 55

Resolution
verified exact
doi, observed 2026-08-07T12:51:50.877031Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:48.485442Z digest=sha256:06b5e93f89a67cc6cf9704c601f138b79a572d81f3d59cc0bebefdb629629e2a

Observation 6b29b74f-12cc-4fe3-bcc7-9e8304446eb3 · outbound

This paper cites Learning from bat: aerodyn amics of actively morphing wing,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Learning from bat: aerodyn amics of actively morphing wing,

Reference 56

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:54.948724Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:48.587682Z digest=sha256:19abfd118d1d749613c97182dbd57acbc13d65c7f9494f9f3a2ddd120a89bbdb

Observation 0c988773-9e4a-4618-b8b5-6988b5cabc85 · outbound

This paper cites Unsteady aerodynamic model of flexible flapping wing,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Unsteady aerodynamic model of flexible flapping wing,

Reference 57

Resolution
verified exact
doi, observed 2026-08-07T12:51:50.714378Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:48.708999Z digest=sha256:67218c760f12b6f4d8be49a86a8c107ab0f86f9fee106eb8f162174814412ccb

Observation 73c30a4a-5b7e-4c16-8be3-7eaf4068bd10 · outbound

This paper cites Vertebrate Flight, volume 27 de Zoophysiology.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Vertebrate Flight, volume 27 de Zoophysiology

Reference 58

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:54.737134Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:48.832646Z digest=sha256:0d5009b1912e0e513c8bd8b8592eb27995703eef754ae179801f78d74060d411

Observation 9492a886-5c53-4ffa-8e97-e0eeb65e9cb6 · outbound

This paper cites Power requirements for horizontal flight in the pigeon Columba livia,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Power requirements for horizontal flight in the pigeon Columba livia,

Reference 59

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:54.530340Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:48.968022Z digest=sha256:c33e628ad6ff0212a8a0d3dfc4fcae3bd9fac9776a0347c1f8133ecf9363800b

Observation 24544664-4f61-478b-a25e-819b50dd47d6 · outbound

This paper cites Unsteady airfoils,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Unsteady airfoils,

Reference 60

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:54.278992Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:49.062175Z digest=sha256:27437fb144e2554818f2977fcbf1cd28eda95be31e36595a31c2d18a36193c04

Observation 9da63642-7e6c-46ef-bfb3-c226857bc9cb · outbound

This paper cites Experiments and numerical simulations on hovering three -dimensional flexible flapping wings,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Experiments and numerical simulations on hovering three -dimensional flexible flapping wings,

Reference 61

Resolution
verified exact
doi, observed 2026-08-07T12:51:50.555508Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:49.155897Z digest=sha256:12a3c467035c9bc88fc29d43c4d785856500c18550a47e24c89868cfc42e551a

Observation a5bf8074-5b3c-40cb-82ad-9a8e0385532b · outbound

This paper cites Effects of wing deformation on aerodynamic forces in hovering hoverflies,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Effects of wing deformation on aerodynamic forces in hovering hoverflies,

Reference 62

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:54.082877Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:49.302094Z digest=sha256:4af88e3719de348a9379fd221a2ff742eb0ab045ea0d2a6b8474171429fc5990

Observation 75522d18-8877-46df-8d72-b319616b07f1 · outbound

This paper cites Flight wing rotation and the aerodynamic basis of insect flight,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Flight wing rotation and the aerodynamic basis of insect flight,

Reference 63

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:53.857484Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:49.414021Z digest=sha256:4c10a7f83f75bafc5a558767a166ff430ffe963728825370ebe062fedff93a50

Observation d988ea31-6375-443a-836a-1da1ef91bab7 · outbound

This paper cites Resonance of flexible flapping wings at low Reynolds number,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Resonance of flexible flapping wings at low Reynolds number,

Reference 64

Resolution
verified exact
doi, observed 2026-08-07T12:51:50.315071Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:49.522402Z digest=sha256:b07b48b542c55858810b2c2d6b2ab21971b37b71223145e83db2e7e2c2eec47c

Observation 1bad4050-834f-44ea-b7a5-400a4aea1a1d · outbound

This paper cites Mechanisms for generating coherent packets of ha irpin vortices in channel flow,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Mechanisms for generating coherent packets of ha irpin vortices in channel flow,

Reference 65

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:53.602277Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:49.637409Z digest=sha256:48d250a5ea7953f75dc0cdfaa66502278b4029b59be5ba5a83f158d1a665632c

Observation 373df258-53b9-4274-a192-9a7175cf61a2 · outbound

This paper cites Eddies, streams, and convergence zones in turbulent flows,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Eddies, streams, and convergence zones in turbulent flows,

Reference 66

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:53.412387Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:49.745545Z digest=sha256:50cbe288f3bd93dcdebf5b14d1e10c793f68b6a0e194b5e2c2a5ad1738f01f4a

Observation 2b4de075-1316-4c78-8a29-1d27f9dc7992 · outbound

This paper cites Vortices behavior depending on the aspect ratio of an insect-like flapping wing in hover,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Vortices behavior depending on the aspect ratio of an insect-like flapping wing in hover,

Reference 67

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:53.142442Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:49.840500Z digest=sha256:31fa1935468bad9093db2e4d021f1660798330a389e0c86b23f7d9bd27c3f453

Observation 00333f6f-ead3-485a-82e0-cb09d64f87ae · outbound

This paper cites Can tip vortices enhance lift of a flapping wing?,.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Can tip vortices enhance lift of a flapping wing?,

Reference 68

Resolution
verified fuzzy
raw_fallback, observed 2026-08-07T12:51:52.919044Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:49.958840Z digest=sha256:c61f7e98f7c67586d913ac83f53c6c554858318f71004281c436d297366c6217

Observation 1e457ecb-6343-4753-bdda-1e5a0242eeb3 · outbound

This paper cites an unresolved cited work.

Lift augmentation by incorporating bend twist coupled composites in flapping wing Unresolved cited work

Reference 69

Resolution
unresolved
raw_fallback, observed 2026-08-07T12:51:52.747345Z

Source-reported events for the cited work

No event found in the named queried sources as of 2026-08-07T06:34:17.273281+00:00.

source=pdf_text observed=2026-08-07T12:51:50.084806Z digest=sha256:1627c9e22dac097c3b98369dd0e880f7cff3cd39780e483b81f46bbeb87a6a3a

Pith citing papers

No inbound Pith citation observations are available.