Ground measurements of the shock-wave noise from supersonic bomber airplanes in the altitude range from 30,000 to 50,000 feet. /
| Main Author: | |
|---|---|
| Corporate Author: | |
| Other Authors: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington, D.C. :
National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce],
[1961]
|
| Series: | NASA technical note ;
D-880 |
| Subjects: |