An analytical method to compute viscous-inviscid transonic flow on axisymmetric afterbodies including jet effects and boattail bleed in separated regions
- 16 August 1975
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- An analytical model of axisymmetric afterbody flow separationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Propulsion Effects on Aerodynamic Characteristics of Lifting Reentry VehiclesPublished by Defense Technical Information Center (DTIC) ,1970
- Two-stream mixing with finite initial boundary layers.AIAA Journal, 1967