Predicting the Influence of Blade Shape on Hover Performance with Comprehensive Analyses
Author:
Affiliation:
1. Continuum Dynamics, Inc., Ewing, New Jersey 08558
Funder
Office of Naval Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/am-pdf/10.2514/1.C034073
Reference21 articles.
1. Hover Predictions on the Sikorsky S-76 Rotor using Helios
2. OVERFLOW Simulation of Rotors in Hover: The Boeing Company
3. Simulation of Rotor in Hover: Current State, Challenges and Standardized Evaluation
4. LeishmanJ. G., Principles of Helicopter Aerodynamics, 2nd ed., Cambridge Univ. Press, Cambridge, England, U.K., 2006, pp. 805–808.
5. BalchD. T.LombardiJ. “Experimental Study of Main Rotor Tip Geometry and Tail Rotor Interactions in Hover. Vol. I—Text and Figures,” NASA CR-177336-Vol-1, 1985.
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