Perturbation Method for Transonic Flows about Oscillating Airfoils
- 1 September 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (9) , 1258-1265
- https://doi.org/10.2514/3.61459
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
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- Convergence acceleration and shock fitting for transonic aerodynamics computationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- A finite difference method for the solution of the transonic flow around harmonically oscillating wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Analysis of Embedded Shock Waves Calculated by Relaxation MethodsAIAA Journal, 1974
- Unsteady transonic flow over oscillating circular-arc airfoilsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- COMPUTATIONAL CONSIDERATIONS IN APPLICATION OF THE FINITE ELEMENT METHOD FOR ANALYSIS OF UNSTEADY FLOW AROUND AIRFOILSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Calculation of plane steady transonic flowsAIAA Journal, 1971
- Inviscid transonic flow over airfoilsAIAA Journal, 1970