Lift and pitching-moment interference between a pointed cylindrical body and triangular wings of various aspect ratios at Mach numbers of 1.50 and 2.02 / Jack N. Nielsen, Elliott D. Katzen, and Kenneth K. Tang.

In order to investigate the effects of interference on wing-body combinations, tests were conducted at Mach nuaibersof 1.50 and 2.02 of a pointed, cylindrical body, of six triangular wings having asyect ratios from 0.67 to 4.00, and of the whgs and the body in combination. The body had a fineness ra...

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Bibliographic Details
Main Author: Nielsen, Jack Norman
Corporate Author: United States. National Advisory Committee for Aeronautics
Other Authors: Katzen, Elliott D., Tang, Kenneth K.
Format: Government Document Book
Language:English
Published: Washington, D.C. : National Advisory Committee for Aeronautics, 1956.
Series:Technical note (United States. National Advisory Committee for Aeronautics) ; 3795.
Subjects:

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Call Number: Y 3.N 21/5:6/3795
Y 3.N 21/5:6/3795 Available Place a Hold