Extension and validation of an unsteady wake model for rotors
- 1 May 1992
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 29 (3) , 374-383
- https://doi.org/10.2514/3.46172
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Finite‐State Induced‐Flow Model for Rotors in Hover and Forward FlightJournal of the American Helicopter Society, 1989
- Technical Note: Dynamic Inflow for Practical ApplicationsJournal of the American Helicopter Society, 1988
- Review of dynamic inflow modeling for rotorcraft flight dynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- A Prescribed Wake Lifting Surface Hover Performance AnalysisJournal of the American Helicopter Society, 1977
- An Analytical Method for Predicting Rotor Wake GeometryJournal of the American Helicopter Society, 1969
- Die kreisförmige Tragfläche auf potentialtheoretischer GrundlageArchive of Applied Mechanics, 1937