Drag Measurements of Symmetrical Circular-arc and NACA 65-009 Rectangular Airfoils Having an Aspect Ratio of 2.7 as Determined by Flight Tests at Supersonic Speeds
07.03.1947
Sonstige
Keine Angabe
Englisch
Maximum lift-to-drag ratio airfoils at moderate supersonic speeds
Engineering Index Backfile | 1969
|