Main rotor free wake geometry effects on blade air loads and response for helicopters in steady maneuvers / by S. Gene Sadler.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Sadler, S. Gene
Corporate Authors:	Rochester Applied Sciences Associates, Langley Research Center, United States. National Aeronautics and Space Administration
Format:	Government Document Book
Language:	English
Published:	Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration ; [For sale by the National Technical Information Service], 1972.
Series:	NASA contractor report ; NASA CR-2110--NASA CR-2111.
Subjects:	Rotors (Helicopters) > Aerodynamics > Mathematical models. Rotors (Helicopters) > Aerodynamics > Computer programs. Wakes (Aerodynamics) > Mathematical models. Wakes (Aerodynamics) > Computer programs.

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