Configuration development of a supersonic cruise strike-fighter
- 16 January 1978
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Comparison of Shock-Induced Two- and Three- Dimensional Incipient Turbulent SeperationAIAA Journal, 1975
- A Simple Correlation for Incipient-Turbulent Boundary-Layer Separation due to a Skewed Shock WaveAIAA Journal, 1973
- Predictions of vortex-lift characteristics by a leading-edge suctionanalogyJournal of Aircraft, 1971
- The Three-Dimensional Interaction of a Shock Wave with a Turbulent Boundary LayerAeronautical Quarterly, 1966
- Types of Flow on Swept Wings With Special Reference to Free Boundaries and Vortex SheetsJournal of the Royal Aeronautical Society, 1953