Behavior of Static Pressure Heads at High Speeds (1938)
NASA Technical Reports Server (NTRS) · leaf 14
Figs. 3,4,5 N.A.C.A.. Technical Memorandum Ho. «65 '10 250 290 330 vCkrn/h""1) Figure 3.- Relation of depth to fly- ing speed with different suspension lengths. … v(kir/ n-1) Figure 4.- Relation of trail to flying speed with different suspension lengths. ?Ug) \/ ' Figure 5.- Tensile stress P lOr ani direction of suspension tubing at airplane body against flying speed with 16 m suspension 200 250 30° 350length vtkm/h-1) 20 18 200 2 50 300 350 vUca/h"1)
NASA Technical Reports Server (NTRS)
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