Inside Out Library · Explore

Airfoil Theory at Supersonic Speed (1939)

NASA Technical Reports Server (NTRS) · leaf 59

An illustration from Airfoil Theory at Supersonic Speed, 1939, leaf 59
S9 Pigs, 15,16,17,18 N.A.C.A. Technical Memorandum No. 897 •Xncbi Figure 15.- Rectangular plane wing. Lift at wing edge. V» t* ps Figure 16.- Polars of plane rectangular wing Figure 17.- Rectangular surface for various aspect ratios. with trapezoidal lift distribution. … Figure 18,- Lifting line with trapesoidal lift distribution. Streamline picture of the y- and s- velocities in a plane at right angles to the axis of the Mach cone.

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

More pictures from Airfoil Theory at Supersonic Speed

More like this