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Far-field acoustic power level and performance analyses of F31/A31 open rotor model at simulated scaled takeoff, nominal takeoff, and approach conditions, technical report I / / Dave Sree
| Far-field acoustic power level and performance analyses of F31/A31 open rotor model at simulated scaled takeoff, nominal takeoff, and approach conditions, technical report I / / Dave Sree |
| Autore | Sree Dave |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , May 2015 |
| Descrizione fisica | 1 online resource (iii, 26 pages) : color illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Rotary wing aircraft
Noise intensity Acoustic measurement Rotor speed Angle of attack |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703877203321 |
Sree Dave
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , May 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Near-field acoustic power level analysis of F31/A31 open rotor model at simulated cruise conditions, technical report II / / Dave Sree
| Near-field acoustic power level analysis of F31/A31 open rotor model at simulated cruise conditions, technical report II / / Dave Sree |
| Autore | Sree Dave |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2015 |
| Descrizione fisica | 1 online resource (iii, 14 pages) : color illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Acoustic measurement
Aerodynamic noise Rotor aerodynamics Noise prediction Sound pressure |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703966103321 |
|
Sree Dave
|
||
| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , July 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||