Ground measurement of the shock-wave noise from supersonic bomber airplanes in the altitude range from 30,000 to 50,000 feet
1961
24 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1961
|Engineering Index Backfile | 1941
|High-Altitude Turbulence For Supersonic Airplanes
NTRS | 1989
|