An improved three-dimensional aerodynamics model for helicopter airloads prediction
- 7 January 1991
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Conservative full-potential model for unsteady transonic rotor flowsAIAA Journal, 1987
- Aeroelastic time response analysis of thin airfoils by transonic code LTRAN2Computers & Fluids, 1981