Analysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed /

Analysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed /

"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 til...

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Bibliographic Details
Main Author: Smith, Arthur F.
Corporate Authors: Lewis Research Center, United Technologies Corporation. Hamilton Standard Division
Format: Government Document Microform Book
Language:English
Published: Windsor Locks, Conn. : Cleveland, Ohio : United Technologies Corporation, Hamilton Standard Division ; National Aeronautics and Space Administration, Lewis Research Center ; 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

Evans: US Documents Microfiche (3rd floor)

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Call Number: NAS 1.26:175026