Three dimensional solution of pneumatic active control of forebody vortex asymmetry
By: Osama A. Kandil and Hazem H. Sharaf El-Din, C.H. Liu.
Contributors: Sharaf El-Din, Hazem H.; Liu, C. H. 1941-.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-203089
Publisher: American Institute of Aeronautics and Astronautics; [National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1995
Place of publication: Washington, D.C; Springfield, Va
Language: eng
Format: Microform
Subjects: Angle of attack.; Finite volume method.; Flux difference splitting.; Forebodies.; Navier-stokes equation.; Pneumatic control.; Tangential blowing.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 97-0824-M.

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