Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 to 20 degrees at high subsonic speeds / Bernard N. Daley and Douglas R. Lord.
Two-dimensional tests of eight 6-percent-thick symmetrical airfoils of the supersonic and subsonic types were conducted in the Langley rectangular high-speed tunnel. Static pressures along the surfaces of each airfoil were measured over a Mach number range from 0.3 to the choking Mach number (about...
Saved in:
| Main Author: | |
|---|---|
| Corporate Author: | |
| Other Authors: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1955.
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3424. |
| Subjects: |
PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3424
|
|---|---|
| Y 3.N 21/5:6/3424 | Available Place a Hold |