Free-flight Investigation of the Zero-lift Drag of Several Wings at Supersonic Mach Numbers Extending to 2.6
1952-12-02
Miscellaneous
No indication
English
Free-flight measurements of zero-lift drag of several wings at Mach numbers from 1.4 to 3.8
Engineering Index Backfile | 1960
|Supersonic wave drag of sweptback tapered wings at zero lift
Engineering Index Backfile | 1947
|