Numerical Calculation of Unsteady Transonic Potential Flow over Helicopter Rotor Blades
- 1 April 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (4), 482-488
- https://doi.org/10.2514/3.61387
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- ANALYSIS OF EMBEDDED SHOCK WAVES CALCULATED BY RELAXATION METHODSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Subsonic and Transonic Potential Flow over Helicopter Rotor BladesAIAA Journal, 1972
- Computation of Transonic Flows past Lifting Airfogs and Slender BodiesAIAA Journal, 1972