Characteristics of deformable leading edge for high performance helicopter rotor
- 9 August 1993
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- A Review of Recent Advances in Computational and Experimental Analysis of Dynamic StallPublished by Springer Nature ,1993
- Numerical Boundary Conditions for Viscous Flow ProblemsAIAA Journal, 1976