WITH reference to the article on the “New Transformed Wing Sections,” by Piercy, Piper and Whitehead, (P) in the November, 1938, number of AIRCRAFT ENGINEERING, it is of interest to note a very simple approximate formula for the symmetrical type of section. This formula is:
The New Type of Aerofoil Section
Further Simplifications, for Designers, of the Formulae for Transformed Wing Sections
Aircraft Engineering and Aerospace Technology ; 11 , 4 ; 151-152
1939-04-01
2 pages
Article (Journal)
Electronic Resource
English
Engineering Index Backfile | 1939
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