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| Format: | Knjiga |
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| era | |
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| format | Book |
| genre | |
| geographic | |
| id | 44c4bdf8-e028-43c4-95ba-0e736bc0178f |
| isbn | |
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| language | eng |
| physical | x, 101/102 p. :ill. |
| publication | – publisher: United Technologies Corporation Hamilton Standard Division dateOfPublication: 1985 |
| publishDate | 1985 |
| subjects | |
| title | Analysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed by Arthur F. Smith. [microform] / |
| topic | Airplanes Airplanes Turbines Propellers 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 |