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نمایش تعداد 1-5 از 5
A Perturbation Method to analyze the effect of cross section and angle of attack for some conical bodies in Hypersonic flow
سال: 2010
خلاصه:
analytically. In order to find lift and drag forces the pressure force on the body is found, the component along x is drag and the component along z is lift. Three equations are obtained for lift to drag ratio of each cross section. The graphs for L/D show...
Comparison of Lift and Drag Forces for Some Conical Bodies in Supersonic Flow Using Perturbation Techniques
سال: 2012
خلاصه:
is lift. Three equations are obtained for lift to drag ratio of each cross section. The graphs for L/D show that for a particular cross section an increase in angle of attack, increases L/D. Comparing L/D in the three mentioned cross sections...