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A Perturbation Method to analyze the effect of cross section and angle of attack for some conical bodies in Hypersonic flow
Year: 2010
Abstract:
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
Year: 2012
Abstract:
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...
Optimal charge control of electric vehicles in parking stations for cost minimization in V2G concept
Publisher: IEEE
Year: 2014