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Unsteady Aerodynamics - Subsonic Compressible Inviscid CaseThis paper presents a new analytical treatment of Unsteady Aerodynamics - the linear theory covering the subsonic compressible (inviscid) case - drawing on some recent work in Operator Theory and Functional Analysis. The specific new results are: (a) An existence and uniqueness proof for the Laplace transform version of the Possio integral equation as well as a new closed form solution approximation thereof. (b) A new representation for the time-domain solution of the subsonic compressible aerodynamic equations emphasizing in particular the role of the initial conditions.
Document ID
19990063634
Acquisition Source
Armstrong Flight Research Center
Document Type
Contractor Report (CR)
Authors
Balakrishnan, A. V.
(California Univ. Los Angeles, CA United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1999
Subject Category
Aerodynamics
Report/Patent Number
H-2337
NASA/CR-1999-206583
NAS 1.26:206583
Funding Number(s)
CONTRACT_GRANT: NCC2-374
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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