Investigation of cross flow shocks on delta wings in supersonic flow
- 15 January 1979
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- A study of the inviscid flow about conically cambered delta wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- A complete numerical technique for the calculation of three-dimensional inviscid supersonic flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Comparison of characteristics and shock capturing methods with application to the space shuttle vehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- A systematic development of the supersonic flow fields over and behind wings and wing-body configurations using a shock-capturing finite-difference approachPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971