Static-thrust measurements of the aerodynamic loading on a helicopter rotor blade / John P. Rabbott, Jr.
An experimental investigation of the aerodynamic loading on a 15-foot-diameter helicopter rotor blade in static thrust was conducted for a tip-speed range of 400 to 500 feet per second and disk loads of zero to about 2.5 pounds per square foot. The chordwise pressure distributions at five spanwise s...
Saved in:
| Main Author: | |
|---|---|
| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1956.
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3688. |
| Subjects: |
PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3688
|
|---|---|
| Y 3.N 21/5:6/3688 | Available Place a Hold |