Simulation of crossflow instability on a supersonic highly swept wing

An edition of Simulation of crossflow instability on a supersonic highly swept wing (1995)

Simulation of crossflow instability on a supersonic highly swept wing

By C. David Pruett

0 (0 Ratings)

0 Want to read0 Currently reading0 Have read

Publish Date

1995

Publisher

National Aeronautics and Space Administration, Langley Research Center,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Computational fluid dynamics, Civil aviation, Three dimensional boundary layer, Cross flow, Flow stability, Runge-Kutta method, Boundary layer transition, Navier-Stokes equation, Incompressible flow, Supersonic speed, Supersonic transports