Computation technique for compressible vortex flows using the integral equation solution
Subtitle: final report
By: by Osama A. Kandil.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA-CR -- 182695.; NASA contractor report -- NASA CR-182695.
Publisher: Dept. of Mechanical Engineering and Mechanics, College of Engineering, Old Dominion University
Published: 1988
Place of publication: Norfolk, Va
Language: eng
Format: Microform
Subjects: Airplanes -- Wings -- Fluid dynamics.; Integral equations.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1988. 1 microfiche.