A full Navier-Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application
By: Kamlesh Kapoor, Bernard H. Anderson, and Robert J. Shaw.
Contributors: Anderson, Bernhard H.; Shaw, Robert J. 1946-; United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 106637.
Publisher: National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1994
Place of publication: [Washington, DC]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Bypasses.; Civil aviation.; Computational fluid dynamics.; Cross flow.; Diffusers.; Flow distortion.; Inlet flow.; Mass flow.; Navier-Stokes equation.; Supersonic diffusers.; Supersonic inlets.; Supersonic transports.
Other titles: Full Navier Stokes analysis of subsonic diffuser of a a bifurcated 70/30 supersonic inlet for high speed civil transport application.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 95-0057-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1994] 1 microfiche.