Report presents the results of drag and pressure tests of spheres having diameters of 2, 4, 6, 8, 10, and 12 inches in eight NACA wind tunnels, in the air ahead of the carriage in the NACA tank, and beneath an autogiro in flight .
Turbulence Factors of NACA Wind Tunnels as Determined by Sphere Tests
01.01.1937
Sonstige
Keine Angabe
Englisch
Turbulence factors of N.A.C.A. wind tunnels as determined by sphere tests
Engineering Index Backfile | 1936
|Turbulence tests of the R.A.E. wind tunnels
TIBKAT | 1935
|Turbulence tests of the R.A.E. wind tunnels
SLUB | 1935
|Tests of inverted spins in NACA free-spinning tunnels
Engineering Index Backfile | 1943
|