AERODYNAMIC STUDY OF SLENDER BODIES WITH NONCIRCULAR CROSS SECTION

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MANI M.; MADANI V.; Khajehfard a.

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Journal: AMIRKABIR Year:2000 | Volume:11 | Issue:44 Page(s): 430-435

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Information Journal Paper

Title

AERODYNAMIC STUDY OF SLENDER BODIES WITH NONCIRCULAR CROSS SECTION

Author(s)

MANI M. | MADANI V. | Khajehfard a. | Issue Writer Certificate

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Abstract

To investigate the aerodynamic characteristics of the slender bodies with non-circular cross sections, two wing-body combinations having identical cross-section areas and lengths, were tested in a wind tunnel at high subsonic, tran-sonic, and supersonic speeds. The results obtained by the tests have pared with the results of the previous written code. Although there are some reasonable differences between them, the code is strong enough to use as a suitable reference for determination of aerodynamic coefficients of these bodies.

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APA: Copy

MANI, M., MADANI, V., & Khajehfard, a.. (2000). AERODYNAMIC STUDY OF SLENDER BODIES WITH NONCIRCULAR CROSS SECTION. AMIRKABIR, 11(44), 430-435. SID. https://sid.ir/paper/1068/en

Vancouver: Copy

MANI M., MADANI V., Khajehfard a.. AERODYNAMIC STUDY OF SLENDER BODIES WITH NONCIRCULAR CROSS SECTION. AMIRKABIR[Internet]. 2000;11(44):430-435. Available from: https://sid.ir/paper/1068/en

IEEE: Copy

M. MANI, V. MADANI, and a. Khajehfard, “AERODYNAMIC STUDY OF SLENDER BODIES WITH NONCIRCULAR CROSS SECTION,” AMIRKABIR, vol. 11, no. 44, pp. 430–435, 2000, [Online]. Available: https://sid.ir/paper/1068/en

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