Dynamic stall control for advanced rotorcraft application

A study investigated advanced concepts designed to improve lift, drag and pitching moment characteristics of rotor blades. The concepts have the potential for substantially improving rotor performance.

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Bibliographic Details
Published in:AIAA journal 1995-02, Vol.33 (2), p.289-295
Main Authors: Yu, Yung H, Lee, Soogab, McAlister, Kenneth W, Tung, Chee, Wang, Clin M
Format: Article
Language:English
Subjects:
Aerodynamics
Aircraft
Applied sciences
Design engineering
Exact sciences and technology
Ground, air and sea transportation, marine construction
Miscellaneous transportation
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Description
Summary:A study investigated advanced concepts designed to improve lift, drag and pitching moment characteristics of rotor blades. The concepts have the potential for substantially improving rotor performance.
ISSN:0001-1452
1533-385X
DOI:10.2514/3.12496