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Avian WingsThis paper describes the avian wing geometry (Seagull, Merganser, Teal and Owl) extracted from non-contact surface measurements using a three-dimensional laser scanner. The geometric quantities, including the camber line and thickness distribution of airfoil, wing planform, chord distribution, and twist distribution, are given in convenient analytical expressions. Thus, the avian wing surfaces can be generated and the wing kinematics can be simulated. The aerodynamic characteristics of avian airfoils in steady inviscid flows are briefly discussed. The avian wing kinematics is recovered from videos of three level-flying birds (Crane, Seagull and Goose) based on a two-jointed arm model. A flapping seagull wing in the 3D physical space is re-constructed from the extracted wing geometry and kinematics.
Document ID
20040075526
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Liu, Tianshu
(NASA Langley Research Center Hampton, VA, United States)
Kuykendoll, K.
(NASA Langley Research Center Hampton, VA, United States)
Rhew, R.
(NASA Langley Research Center Hampton, VA, United States)
Jones, S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2004
Subject Category
Aerodynamics
Report/Patent Number
AIAA Paper 2004-2186
Report Number: AIAA Paper 2004-2186
Meeting Information
Meeting: 24th AIAA Aerodynamic Measurement Technology and Ground Testing Conference
Location: Portland, OR
Country: United States
Start Date: June 28, 2004
End Date: July 1, 2004
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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