Flight Tests to Determine the Effect of Airfoil Section Profile and Thickness Ratio on the Zero-Lift Drag of Low-Aspect Ratio Wings at Supersonic Speeds
1948
19 pages
Report
No indication
English
Engineering Index Backfile | 1956
|Effect of aspect ratio and taper on pressure drag at supersonic speeds of unswept wings at zero lift
Engineering Index Backfile | 1947
|