In-flight shock wave pressure measurements above and below bomber aircraft at mach 1.42 to 1.69
IN-FLIGHT SHOCK-WAVE PRESSURE MEASUREMENTS ABOVE AND BELOW A BOMBER AIRPLANE AT MACH NUMBERS FROM 1.42 TO 1.69
1963-10-01
Miscellaneous
No indication
English
Flight characteristics of B-58 mach 2 bomber
Engineering Index Backfile | 1962
|Engineering Index Backfile | 1960
|