Analysis of unsteady inviscid diffuser flow with a shock wave
- 1 May 1985
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 1 (3) , 222-228
- https://doi.org/10.2514/3.22784
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- The Response of Normal Shocks in DiffusersAIAA Journal, 1983
- Characteristic frequencies of transonic diffuser flow oscillationsAIAA Journal, 1983
- Numerical solution of the Navier-Stokes equations for compressible turbulent two/three dimensional flows in the terminal shock region of an inlet/diffuserPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Analysis of viscous-inviscid interaction in transonic internal flowsAIAA Journal, 1983
- Boundary Condition Specification for Mobile Granular Propellant Bed Combustion ProcessesAIAA Journal, 1981
- Shock-Wave Oscillations in a Transonic Diffuser FlowAIAA Journal, 1979
- Large Amplitude Shock-Wave Motion in Two-Dimensional, Transonic Channel FlowsAIAA Journal, 1978