The Wake Geometry of a Hovering Helicopter Rotor and Its Influence on Rotor Performance
- 1 October 1972
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 17 (4) , 3-15
- https://doi.org/10.4050/jahs.17.3
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Wake and boundary layer effects in helicopter rotor aerodynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1971
- An Analytical and Experimental Investigation of Helicopter Rotor Hover Performance and Wake Geometry CharacteristicsPublished by Defense Technical Information Center (DTIC) ,1971
- The Free Wake AnalysisJournal of the American Helicopter Society, 1970
- An Analytical Method for Predicting Rotor Wake GeometryJournal of the American Helicopter Society, 1969
- A Reassessmemt of Rotor Hovering Performance Prediction MethodsJournal of the American Helicopter Society, 1968
- AN AERODYNAMIC ANALYSIS OF A SINGLEBLADED ROTOR IN HOVERING AND LOW- SPEED FORWARD FLIGHT AS DETERMINED FROM SMOKE STUDIES OF THE VORTICITY DISTRIBUTION IN THE WAKEPublished by Defense Technical Information Center (DTIC) ,1956