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...
| Uniform Title: | NASA contractor report ;
NASA CR-175026. |
|---|---|
| Main Author: | |
| Corporate Authors: | |
| 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.
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| Series: | NASA contractor report ;
NASA CR-175026. |
| Subjects: | |
| Physical Description: | x, 101/102 pages : illustrations. Distributed to depository libraries in microfiche; also available online. |
| Format: | Government Document Microfilm Book |