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Works on theory of flapping wingIt is shown mathematically that taking account of the boundary layer is the only way to develop a theory of flapping wings without violating the basic observations and mathematics of hydromechanics. A theory of thrust generation by flapping wings can be developed if the conventional downstream velocity discontinuity surface is replaced with the observed Karman type vortex streets behind a flapping wing. Experiments show that the direction of such vortices is the reverse of that of conventional Karman streets. The streets form by breakdown of the boundary layer. Detailed analysis of the movements of certain birds and insects during flight 'in place' is fully consistent with this theory of the lift, thrust and drag of flapping wings. Further directions for research into flight with flapping wings are indicated.
Document ID
19800017776
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Golubev, V. V.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1980
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-75750
Report Number: NASA-TM-75750
Accession Number
80N26275
Funding Number(s)
CONTRACT_GRANT: NASW-3199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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