Noise survey under static conditions of a turbine-driven full-scale modified supersonic propeller with an advance ratio of 3.2 / Max C. Kurbjun.
Overall sound-pressure levels and frequency spectra have been obtained under static conditions from a modified supersonic propeller designed to operate efficiently at a high forward speed without the high noise levels associated with the supersonic propeller. The three-blade, 10-foot-diameter, 1,700...
Saved in:
| Main Author: | |
|---|---|
| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
[1958]
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
4172. |
| Subjects: |
PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/4172
|
|---|---|
| Y 3.N 21/5:6/4172 | Available Place a Hold |