Studies on Blade‐to‐Blade and Rotor‐Fuselage‐Tail Interferences
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Publisher
Emerald
Reference20 articles.
1. APPROXIMATE SOLUTIONS FOR COMPUTING HELICOPTER HARMONIC AIRLOADS
2. Joglekar, M., Lowey, R. An Actuator-Disc Analysis of Helicopter Wake Geometry and the Corresponding Blade Response, USAAVLABS Technical Report 69-66, 1970.
3. Landgrebe, A. J. An Analytical and Experimental Investigation of Helicopter Rotor Hover Performance and Wake Geometry Characteristics, USAAMRDL Technical Report 71-24, 1971.
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