Euler analysis of a High-Speed Civil Transport concept at Mach 3
- 1 April 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 28 (4) , 239-245
- https://doi.org/10.2514/3.46018
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Full-potential analysis of a supersonic delta wing/bodyJournal of Aircraft, 1989
- A hybrid finite volume approach to Euler solutions for supersonic flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Real flow limitations in supersonic airplane designPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- A Simple Correlation for Incipient-Turbulent Boundary-Layer Separation due to a Skewed Shock WaveAIAA Journal, 1973
- Aerodynamic design integration of supersonic aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1968