The Pressure Distribution over the Horizontal Tail Surfaces of an Airplane III (1923)
NASA Technical Reports Server (NTRS) · leaf 24
ISTRIBUTION OVKR HORIZONTAL TAIL STRFACLS. tlie (Mid reaches the high value1 of (>.0 pounds per square foot, corresponding in time to the maximum acceleration. The results from this case show that the loading in the spin itself is noi SO great as in flatten- ing out quickly from an 80 mile an hour… … Time in seconds Fig. 28.—Tail spin. STRESSES DUE TO TAIL-PLANE LOAD. PRESENT METHOD OF COMPUTING TAIL-PLANE LOAD. It has been usually assumed hitherto that the horizontal tail surfaces received the greatest load when flattening out of a dive and that this load acted downward. The method of com-…
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