Investigation of minimum drag and maximum lift-drag ratios of several wing-body combinations including a cambered triangular wing at low Reynolds numbers and at supersonic speeds / Clinton E. Brown and L.K. Hargrave.
Theoretical and experimental data for wing-body combinations with wings of triangular, arrow, and diamond plan form are presented for Mach numbers of 1.62, 1.93, and 2.41 and a Reynolds number range of 1.4 x 10 to the 6th power to 0.7 x 10 to the 6th power. Included are two each of triangular and ar...
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| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
[1958]
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| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
4020. |
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PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/4020
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| Y 3.N 21/5:6/4020 | Available Place a Hold |