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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Format: | Government Document Book |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1956.
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3795. |
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Call Number: |
Y 3.N 21/5:6/3795
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Y 3.N 21/5:6/3795 | Available Place a Hold |