Experimental investigation of effects of blade tip geometry on loads and performance for an articulated rotor system / William H. Weller, Structures Laboratory, AVRADCOM Research and Technology Laboratories, Langley Research Center.

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Bibliographic Details
Online Access:	Search for the full-text version of this title in HathiTrust
Main Author:	Weller, William H.
Corporate Authors:	Army Research and Technology Laboratories (U.S.). Structures Laboratory, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Format:	Government Document Book
Language:	English
Published:	[Washington] : Springfield, Va. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; For sale by the National Technical Information Service, 1979.
Series:	AVRADCOM technical report ; 78-53 NASA technical paper ; 1303.
Subjects:	Rotors (Helicopters) Helicopters > Models > Testing. Aerodynamic load.

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Holdings details from Norlin Library - Government Information - US
Call Number:	NAS 1.60:1303
NAS 1.60:1303	Available Place a Hold