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Three-dimensional unsteady lifting surface theory in the subsonic rangeThe methods of the unsteady lifting surface theory are surveyed. Linearized Euler's equations are simplified by means of a Galileo-Lorentz transformation and a Laplace transformation so that the time and the compressibility of the fluid are limited to two constants. The solutions to this simplified problem are represented as integrals with a differential nucleus; these results in tolerance conditions, for which any exact solution must suffice. It is shown that none of the existing three-dimensional lifting surface theories in subsonic range satisfy these conditions. An oscillating elliptic lifting surface which satisfies the tolerance conditions is calculated through the use of Lame's functions. Numerical examples are calculated for the borderline cases of infinitely stretched elliptic lifting surfaces and of circular lifting surfaces. Out of the harmonic solutions any such temporal changes of the down current are calculated through the use of an inverse Laplace transformation.
Document ID
19850012801
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kuessner, H. G.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-77812
NAS 1.15:77812
Report Number: NASA-TM-77812
Report Number: NAS 1.15:77812
Meeting Information
Meeting: European Aeron. Congr.
Location: Scheveningen
Country: Netherlands
Start Date: September 25, 1956
End Date: September 29, 1956
Accession Number
85N21111
Funding Number(s)
CONTRACT_GRANT: NASW-4006
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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