Analytical Prediction of Vortex‐Ring Boundaries for Helicopters in Steep Descents
- 1 July 1972
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 17 (3) , 13-19
- https://doi.org/10.4050/jahs.17.13
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Stability and Control of Helicopters in Steep Approaches. Volume 1. Summary rept.Published by Defense Technical Information Center (DTIC) ,1971
- Induced flow variation of the helicopter rotor operating in the vortex ring state.Journal of Aircraft, 1968
- Experiments on a model helicopter rotor operating in the vortex ringstate.Journal of Aircraft, 1966
- EXPERIMENTAL STUDY ON THE UNSTEADY AERODYNAMICS OF A MODEL HELICOPTER ROTOR OPERATING IN THE VORTEX RING STATEPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1965