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Analysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed [[electronic resource] /] / by Arthur F. Smith
| Analysis and test evaluation of the dynamic response and stability of three advanced turboprop models at low forward speed [[electronic resource] /] / by Arthur F. Smith |
| Autore | Smith Arthur F |
| Pubbl/distr/stampa | Windsor Locks, Conn. : , : Hamilton Standard Division, United Technologies Corporation |
| Descrizione fisica | 1 online resource (x, 101/102 pages) : illustrations |
| Collana | NASA CR |
| Soggetto topico |
Aerodynamic stability
Dynamic response Dynamic structural analysis Evaluation Prop-fan technology Turboprop engines |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701902203321 |
Smith Arthur F
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| Windsor Locks, Conn. : , : Hamilton Standard Division, United Technologies Corporation | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Analysis and test evaluation of the dynamic stability of three advanced turboprop models at zero forward speed [[electronic resource] /] / by Arthur F. Smith
| Analysis and test evaluation of the dynamic stability of three advanced turboprop models at zero forward speed [[electronic resource] /] / by Arthur F. Smith |
| Autore | Smith Arthur F |
| Pubbl/distr/stampa | Windsor Locks, Conn. : , : Hamilton Standard Division, United Technologies Corporation |
| Descrizione fisica | 1 online resource (ix/x, 114 pages) : illustrations |
| Collana | NASA CR |
| Soggetto topico |
Dynamic stability
Evaluation Prop-fan technology Turboprop engines Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910701902003321 |
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Smith Arthur F
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| Windsor Locks, Conn. : , : Hamilton Standard Division, United Technologies Corporation | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Analytical fuel property effects Small combustors . Phase 2 [[electronic resource] ] : final report / / by J. Monty and T. Scott ; prepared for National Aeronautics and Space Administration, Lewis Research Center
| Analytical fuel property effects Small combustors . Phase 2 [[electronic resource] ] : final report / / by J. Monty and T. Scott ; prepared for National Aeronautics and Space Administration, Lewis Research Center |
| Autore | J. Monty |
| Pubbl/distr/stampa | Lynn, MA : , : Aircraft Engine Business Group, General Electric, , [1985] |
| Descrizione fisica | 1 online resource (iv, 39 pages) |
| Altri autori (Persone) | ScottT |
| Collana | NASA CR |
| Soggetto topico |
Aircraft engines
Combustion chambers Diesel fuels Engine design Exhaust emission Gas analysis Jet engine fuels Smoke Surface temperature Turboprop engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Analytical fuel property effects |
| Record Nr. | UNINA-9910700283903321 |
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J. Monty
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| Lynn, MA : , : Aircraft Engine Business Group, General Electric, , [1985] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Piloted simulation study of an ILS approach of a twin-pusher business/commuter turboprop aircraft configuration / / Donald R. Riley and Jay M. Brandon, Louis J. Glaab
| Piloted simulation study of an ILS approach of a twin-pusher business/commuter turboprop aircraft configuration / / Donald R. Riley and Jay M. Brandon, Louis J. Glaab |
| Autore | Riley Donald R. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , January 1994 |
| Descrizione fisica | 1 online resource (118 pages, 1 unnumbered page) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aircraft landing
Aerodynamics Turboprop engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Piloted simulation study of an instrument landing system approach of a twin-pusher business/commuter turboprop aircraft configuration |
| Record Nr. | UNINA-9910716644803321 |
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Riley Donald R.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , January 1994 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Soggetto topico
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Turboprop engines
(4)
- Evaluation (2)
- Prop-fan technology (2)
- Aerodynamic stability (1)
- Aerodynamics (1)