| |
|
|
|
|
|
|
|
|
1. |
Record Nr. |
UNINA9910716550903321 |
|
|
Autore |
Smeltzer Donald B. |
|
|
Titolo |
Tests of a mixed compression axisymmetric inlet with large transonic mass flow at Mach numbers 0.6 to 2.65 / / by Donald B. Smeltzer and Norman E. Sorensen |
|
|
|
|
|
|
|
Pubbl/distr/stampa |
|
|
Washington, D.C. : , : National Aeronautics and Space Administration, , December 1972 |
|
|
|
|
|
|
|
|
|
Descrizione fisica |
|
1 online resource (v, 183 pages) : illustrations |
|
|
|
|
|
|
Collana |
|
|
|
|
|
|
Soggetti |
|
Jet engines |
Mach number |
Propulsion |
Jet engines - Air intakes |
Aerodynamics, Transonic |
|
|
|
|
|
|
|
|
Lingua di pubblicazione |
|
|
|
|
|
|
Formato |
Materiale a stampa |
|
|
|
|
|
Livello bibliografico |
Monografia |
|
|
|
|
|
Note generali |
|
|
|
|
|
|
Nota di bibliografia |
|
Includes bibliographical references (page 26). |
|
|
|
|
|
| |