An extensive experimental investigation to understand the aerodynamic behavior of wrap around fin (WAF) missile configuration has been conducted. Various tests using at first a standard model (TTCP) in the trisonic wind tunnel of Imam Hossein University has been performed. The tunnel has attest section of 60×60 cm2 and can operate at Mach numbers of 0.4≤M∞≤2.2 and at attack angles of -4˚≤α≤10˚. 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.
Keywords: Wind tunnel, Wrap around fin, Missile, Balance WAF-TTCP
M. R. Soltani, , H. Fazeli, , & B. Farahanieh and A. R. Davari, (2022). An Experimental Study of the Aerodynamic Behavior of the Two Wrap Around Fin Missiles. Journal of Advanced Materials in Engineering (Esteghlal), 21(1), 141-152.
MLA
M. R. Soltani; H. Fazeli; B. Farahanieh and A. R. Davari. "An Experimental Study of the Aerodynamic Behavior of the Two Wrap Around Fin Missiles", Journal of Advanced Materials in Engineering (Esteghlal), 21, 1, 2022, 141-152.
HARVARD
M. R. Soltani, , H. Fazeli, , B. Farahanieh and A. R. Davari, (2022). 'An Experimental Study of the Aerodynamic Behavior of the Two Wrap Around Fin Missiles', Journal of Advanced Materials in Engineering (Esteghlal), 21(1), pp. 141-152.
VANCOUVER
M. R. Soltani, , H. Fazeli, , B. Farahanieh and A. R. Davari, An Experimental Study of the Aerodynamic Behavior of the Two Wrap Around Fin Missiles. Journal of Advanced Materials in Engineering (Esteghlal), 2022; 21(1): 141-152.
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