Nonlinear stability of supersonic jets
Subtitle: final report
By: by T.R.S. Bhat and S.N. Tiwari, principal investigator ; submitted by the Old Dominion University Research Foundation.
Contributors: Tiwari, S. N.; Old Dominion University. Research Foundation.; United States. National Aeronautics and Space Administration.
Series: NASA contractor report -- NASA CR-202199
Publisher: Dept. of Mechanical Engineering, College of Engineering & Technology, Old Dominion University; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1996
Place of publication: Norfolk, Va; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Subjects: Supersonic jet flow.; Aerodynamic stability.; Nonlinearity.; Parabolic differential equations.; Parallel flow.; Rayleigh equations.; Operating temperature.; Aircraft structures.; Linearity.; Aerodynamic noise.; Shock waves.; Jet aircraft noise.; Navier-Stokes equation.
Notes: Shipping list no.: 98-0983-M.

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