Computation of Transonic Flow about Finite Lifting Wings
- 1 July 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (7) , 971-973
- https://doi.org/10.2514/3.50274
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
- Solution of the transonic potential equation using a mixed finite difference systemPublished by Springer Nature ,2008
- Vortex-elliptic wing interaction.AIAA Journal, 1972
- Relaxation techniques for three-dimensional transonic flow about wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972
- Transonic Flow about Two-Dimensional Airfoils by Relaxation ProceduresAIAA Journal, 1972
- Analysis of transonic airfoilsCommunications on Pure and Applied Mathematics, 1971
- Solution of the lifting line equation for twisted elliptic wingsJournal of Aircraft, 1971
- Helicopter Noise due to Blade-Vortex InteractionThe Journal of the Acoustical Society of America, 1971
- Calculation of plane steady transonic flowsAIAA Journal, 1971