Far-field turbulent vortex-wake/exhaust plume interaction for subsonic and HSCT airplanes
Subtitle: 27th AIAA Fluid Dynamics Conference, June 17-20, 1996/New Orleans, LA
By: Osama A. Kandil, Ihab Adam and Tin-Chee Wong.
Contributors: Adam, Ihab.; Wong, Tin Chee.; American Institute of Aeronautics and Astronautics.; United States. National Aeronautics and Space Administration.
Series: [NASA contractor report] -- NASA-CR-203260.
Publisher: American Institute of Aeronautics and Astronautics; [National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Turbulent flow.; Vortices.; Navier-Stokes equation.; Supersonic transports.; Finite difference theory.; Shear stress.; Turbulent wakes.
Other titles: Far field turbulent vortex wake, exhaust plume interaction for subsonic and HSCT airplanes.
Notes: Shipping list no.: 98-1104-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.