Calculations, based on wind tunnel tests at fairly high Reynolds number, indicate that, for high speed airplane having fuselage, wings, and fixed tail units of Duramold, 25% less power will be required at given high speed than for all metal airplane. Before Soc Automotive Engrs, World Automotive Eng Congress.
"Plastic" airplane
Mech Eng
Mechanical Engineering ; 61 , n 7
1939
Article (Journal)
English
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