|
|
|
|
|
|
|
|
1. |
Record Nr. |
UNINA9910714050603321 |
|
|
Autore |
Weirich Robert L. |
|
|
Titolo |
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 |
|
|
|
|
|
|
|
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 ; ; TN D-4809 |
|
|
|
|
|
|
Soggetti |
|
Supersonic wind tunnels - Testing |
Supersonic planes - Design and construction |
Supersonic planes - Testing |
|
|
|
|
|
|
|
|
Lingua di pubblicazione |
|
|
|
|
|
|
Formato |
Materiale a stampa |
|
|
|
|
|
Livello bibliografico |
Monografia |
|
|
|
|
|
Note generali |
|
|
|
|
|
|
Nota di bibliografia |
|
Includes bibliographical references (page 12). |
|
|
|
|
|