Experimental investigation of temperature recovery factors on a 10 degree cone at angle of attack at a Mach number of 3.12 / John R. Jack and Barry Moskowitz.
Temperature recovery factors on a thin-walled, metal, 10 degree included angle cone were obtained at a Mach number of 3.12 over a range of angles of attack from 0 to 10 degrees and for Reynolds numbers per foot from 1,500,000 to 8,000,000. Over the Reynolds number range investigated, an increase in...
Saved in:
| Main Author: | |
|---|---|
| Corporate Author: | |
| Other Authors: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
[1954]
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3256. |
| Subjects: |
PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3256
|
|---|---|
| Y 3.N 21/5:6/3256 | Available Place a Hold |