Some design considerations for supersonic cruise mixed compression inlets
- 16 August 1973
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Bleed System Design Technology for Supersonic InletsJournal of Aircraft, 1973
- Advanced supersonic inlet technology.Journal of Aircraft, 1973
- Performance Estimates for a Supersonic Axisymmetric Inlet SystemJournal of Aircraft, 1972
- Combined Viscous-Inviscid Analysis of Supersonic Inlet FlowfieldsJournal of Aircraft, 1972
- Shock-wave reflection from a turbulent boundary layer with mass bleed.Journal of Aircraft, 1968