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Flow-field properties near an arrow-wing--body model at Mach numbers of 1.60, 2.36, and 2.96 / / by Robert L. Weirich and Walter A. Vahl
| Flow-field properties near an arrow-wing--body model at Mach numbers of 1.60, 2.36, and 2.96 / / by Robert L. Weirich and Walter A. Vahl |
| Autore | Weirich Robert L. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , October 1968 |
| Descrizione fisica | 1 online resource (135 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Supersonic wind tunnels - Testing
Supersonic planes - Design and construction Supersonic planes - Testing |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910714050603321 |
Weirich Robert L.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , October 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Investigation of a class of bodies that generate far-field sonic-boom shock strength and impulse independent of body length and volume / / by Raymond L. Barger and Frank L. Jordan, Jr
| Investigation of a class of bodies that generate far-field sonic-boom shock strength and impulse independent of body length and volume / / by Raymond L. Barger and Frank L. Jordan, Jr |
| Autore | Barger Raymond L. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , May 1969 |
| Descrizione fisica | 1 online resource (15 pages) : illustrations |
| Collana | NASA technical note |
| Soggetto topico |
Supersonic planes - Design and construction
Airplanes - Noise - Evaluation Sonic boom - Evaluation |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713918503321 |
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Barger Raymond L.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , May 1969 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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