Combined Viscous-Inviscid Analysis of Supersonic Inlet Flowfields
- 1 August 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 9 (8) , 589-595
- https://doi.org/10.2514/3.59041
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Performance Estimates for a Supersonic Axisymmetric Inlet SystemJournal of Aircraft, 1972
- The interaction of a shock wave with a laminar boundary layer†International Journal of Non-Linear Mechanics, 1968