Numerical calculation of unsteady transonic potential flow over helicopter rotor blades
- 20 January 1975
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- ANALYSIS OF EMBEDDED SHOCK WAVES CALCULATED BY RELAXATION METHODSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Computation of Transonic Flows past Lifting Airfogs and Slender BodiesAIAA Journal, 1972