An Improved Mach-Box Approach for Supersonic Oscillatory Pressures
- 1 September 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 14 (9) , 887-893
- https://doi.org/10.2514/3.58869
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Oscillatory supersonic kernel function method for interfering surfacesJournal of Aircraft, 1974
- High Speed Wing TheoryPublished by Walter de Gruyter GmbH ,1960
- Aerodynamic Flutter Derivatives for a Flexible Wing with Supersonic and Subsonic EdgesJournal of the Aeronautical Sciences, 1955