AN EXPERIMENTAL STUDY OF THE AERODYNAMIC BEHAVIOR OF TWO WRAP AROUND FIN MISSILES

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SOLTANI M.R.; FAZELI H.; FARAHANIEH B.; DAVARI A.R.

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Paper Information

Journal: ESTEGHLAL Year:2002 | Volume:21 | Issue:1 Page(s): 141-152

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Information Journal Paper

Title

AN EXPERIMENTAL STUDY OF THE AERODYNAMIC BEHAVIOR OF TWO WRAP AROUND FIN MISSILES

Author(s)

SOLTANI M.R. | FAZELI H. | FARAHANIEH B. | DAVARI A.R. | Issue Writer Certificate

Keywords

WIND TUNNELQ2

WARP AROUND FINQ4

MISSILEQ3

BALANCE WAF-TTCPQ4

Abstract

An extensive experimental investigation to understand the aerodynamic behavior of wrap around in (WAF) MISSILE configuration has been conducted Various tests using at first a standard model (TTCP)in the transonic WIND TUNNEL of Imam Rouein University has been performed The tunnel has a test section of 60´60 cm and can operate at Mach numbers of 0.4 £ M¥£ 2.2 and at attack angles of - 4° £a£100. Experimental longitudinal results are compared with those of NASA and an engineering code. The results for TTCP model are in good agreement. After gaining confidence on the TTCP results, a new model of WAF rocket was designed, built and tested this paper compares the results of two models tested under the same conditions.

Cites

EXPERIMENTAL INVESTIGATIONS OF SUPERSONIC FLOW AROUND A LONG AXISYMMETRIC BODY

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APA: Copy

SOLTANI, M.R., FAZELI, H., FARAHANIEH, B., & DAVARI, A.R.. (2002). AN EXPERIMENTAL STUDY OF THE AERODYNAMIC BEHAVIOR OF TWO WRAP AROUND FIN MISSILES. ESTEGHLAL, 21(1), 141-152. SID. https://sid.ir/paper/371640/en

Vancouver: Copy

SOLTANI M.R., FAZELI H., FARAHANIEH B., DAVARI A.R.. AN EXPERIMENTAL STUDY OF THE AERODYNAMIC BEHAVIOR OF TWO WRAP AROUND FIN MISSILES. ESTEGHLAL[Internet]. 2002;21(1):141-152. Available from: https://sid.ir/paper/371640/en

IEEE: Copy

M.R. SOLTANI, H. FAZELI, B. FARAHANIEH, and A.R. DAVARI, “AN EXPERIMENTAL STUDY OF THE AERODYNAMIC BEHAVIOR OF TWO WRAP AROUND FIN MISSILES,” ESTEGHLAL, vol. 21, no. 1, pp. 141–152, 2002, [Online]. Available: https://sid.ir/paper/371640/en

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