An efficient supersonic wind tunnel drive system for Mach 2.5 flows
- 17 August 1991
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- The compressible turbulent shear layer: an experimental studyJournal of Fluid Mechanics, 1988
- A mathematically simple turbulence closure model for attached and separated turbulent boundary layersAIAA Journal, 1985
- Implicit Finite-Difference Simulation of Flow about Arbitrary Two-Dimensional GeometriesAIAA Journal, 1978