Analysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed / by Arthur F. Smith.

"Results of wind tunnel tests at low forward speed for blade dynamic response and stability of three 62.2 cm (24.5 in) diameter models of the Prop-Fan, advanced turboprop, are presented. Measurements of dynamic response were made with the rotors mounted on an isolated nacelle, with varying tilt for...

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Bibliographic Details
Uniform Title:	NASA contractor report ; NASA CR-175026.
Main Author:	Smith, Arthur F.
Corporate Authors:	Lewis Research Center United Technologies Corporation. Hamilton Standard Division
Language:	English
Published:	Windsor Locks, Conn. : Cleveland, Ohio : [Springfield, Va.] : United Technologies Corporation, Hamilton Standard Division ; National Aeronautics and Space Administration, Lewis Research Center ; [For sale by the National Technical Information Service], 1985.
Series:	NASA contractor report ; NASA CR-175026.
Subjects:	Airplanes > Turbine-propeller engines > Blades > Testing. Airplanes > Turbojet engines > Blades > Testing. Turbines > Blades > Testing. Propellers > Aerodynamics > Testing. Aerodynamic stability. Dynamic response. Dynamic structural analysis. Evaluation. Prop-fan technology. Turboprop engines. Propeller fans. Prop-fan technology; Turboprop engines; Nacelles; Rotors; Aerodynamic stability; Dynamic response; Dynamic structural analysis; Aerodynamic stalling; Flutter analysis; Installing; Mach number; Wind tunnel models; Wind tunnel tests; Evaluation; Finite element method.
Physical Description:	x, 101/102 pages : illustrations. Distributed to depository libraries in microfiche; also available online.
Format:	Government Document Microfilm Book

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