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Experimental and mathematical simulation of fairing aircraft with braking devices
Engineering Education # 11, November 2012
DOI: 10.7463/1112.0489665
The purpose of this work is to determine the influence of design parameters, such as a form of the fairing, lengthening of the body, type of brakes, on aerodynamic characteristics and flow structure of an aircraft. This paper presents the results of physical experiments on the flow around aircraft with different configurations of the bow and braking. Numerical calculations of the studied bodies and comparative analysis of the results were conducted. Problem formulation and method of calculation were described. The Reynolds equations were closed using the k-omega SST turbulence model. The solution method is based on the finite method algorithm. The influence of gas flow between the plates on the value of the base drag was revealed.
 
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