Theoretical and Experimental Investigation of Second-Order Supersonic Wing-Body Interference
- 1 September 1960
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 27 (9) , 694-702
- https://doi.org/10.2514/8.8711
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Unsteady Flow Around Thin Wings at High Mach NumbersJournal of the Aeronautical Sciences, 1957
- The Generalized Shock-Expansion Method and Its Application to Bodies Traveling at High Supersonic Air SpeedsJournal of the Aeronautical Sciences, 1955
- Applications of Hypersonic Small-Disturbance TheoryJournal of the Aeronautical Sciences, 1954
- Oscillating Airfoils at High Mach NumberJournal of the Aeronautical Sciences, 1953