Correlation of SA349/2 Helicopter Flight Test Data with a Comprehensive Rotorcraft Model
- 1 April 1988
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 33 (2), 31-42
- https://doi.org/10.4050/jahs.33.31
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Effect of helicopter blade dynamics on blade aerodynamic and structural loadsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Numerical modeling of rotor flows with a conservative form of the full-potential equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Torsion of Pretwisted Beams Due to Axial LoadingJournal of Applied Mechanics, 1980
- Prediction of Control Loads Due to Blade StallJournal of the American Helicopter Society, 1972
- Rotor High Speed Performance, Theory vs. TestJournal of the American Helicopter Society, 1970