|
|
|
|
|
|
|
|
|
1. |
Record Nr. |
UNINA9910716080803321 |
|
|
Autore |
Stainback P. Calvin |
|
|
Titolo |
Effect of unit Reynolds number, nose bluntness, angle of attack, and roughness on transition on a 5° half-angle cone at Mach 8 / / by P. Calvin Stainback |
|
|
|
|
|
|
|
Pubbl/distr/stampa |
|
|
Washington, D.C. : , : National Aeronautics and Space Administration, , January 1969 |
|
|
|
|
|
|
|
|
|
Descrizione fisica |
|
1 online resource (76 pages) : illustrations |
|
|
|
|
|
|
Collana |
|
|
|
|
|
|
Soggetti |
|
Reynolds number |
Aerodynamics |
Mach number |
Aerodynamics, Hypersonic |
Angle of attack (Aerodynamics) |
Noses (Space vehicles) |
|
|
|
|
|
|
|
|
Lingua di pubblicazione |
|
|
|
|
|
|
Formato |
Materiale a stampa |
|
|
|
|
|
Livello bibliografico |
Monografia |
|
|
|
|
|
Note generali |
|
|
|
|
|
|
Nota di bibliografia |
|
Includes bibliographical references (pages 24-27). |
|
|
|
|
|
| |