Simulation of crossflow instability on a supersonic highly swept wing
By: C. David Pruett.
Contributors: Langley Research Center.
Series: NASA contractor report -- 198267.; NASA contractor report -- NASA CR-198267.
Publisher: National Aeronautics and Space Administration, Langley Research Center; National Technical Information Service, distributor
Published: 1995
Place of publication: Hampton, Va; [Springfield, Va
Language: eng
Format: Microform
Subjects: Boundary layer transition.; Civil aviation.; Computational fluid dynamics.; Cross flow.; Flow stability.; Incompressible flow.; Navier-Stokes equation.; Runge-Kutta method.; Supersonic speed.; Supersonic transports.; Three dimensional boundary layer.
Notes: Distributed to depository libraries in microfiche.

Shipping list no.: 96-0513-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1996] 1 microfiche.