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
© Metadata Copyright Elsevier B. V. All rights reserved.
Engineering Index Backfile | 1942
|Development of plastic molded airplane
Engineering Index Backfile | 1941
|Collecting vintage plastic model airplane kits
TIBKAT | 2015
|Plastic airplane parts stand test of time
Engineering Index Backfile | 1944
Engineering tests of T14 plastic airplane landing mat
Engineering Index Backfile | 1967
|