It has been shown that the problem of finding minimum drag configuration in hypersonic flow can be reduced to a problem in optimum control and the method of steepest ascent is a useful tool for finding the solution of this problem
Abstract. The problem on the configuration with maximum lift-to-drag ratio in supersonic gas flow is...
Optimum body length and volume design for minimal drag characteristics of hypersonic aircraf
The present work takes origin from studies carried out at the Department of Aerospace Engineering of...
It has been shown that the problem of finding minimum drag configuration in hypersonic flow can be ...
A unified treatment is given to the problem of finding minimum total drag bodies-both two-dimensiona...
Variational calculus methods for drag reduction of lifting bodies in hypersonic flo
Optimum contours for internaI shapes in Newtonian hypersonic flow with constant and variable skin fr...
A new method was developed to optimize, in terms of aerodynamic wave drag minimization, arbitrary (n...
Control programs and flight paths of a hypersonic vehicle in climb are analyzed. Two approaches to s...
. In this paper, a method based on the optimal control theory for the solution of shape optimization...
This paper presents the classic approach to minimum drag shape body problem, moving at hypersonic sp...
By use of an approximate equation for the wave drag of slender bodies of revolution in a supersonic ...
Abstract. The efficient direct optimization method for supersonic aircraft design is presented. The ...
A theoretical investigation is made of the airfoil profile for minimum pressure drag at zero lift in...
Analytical solutions for variational problems on configurations of threedimensional (3D) bodies with...
Abstract. The problem on the configuration with maximum lift-to-drag ratio in supersonic gas flow is...
Optimum body length and volume design for minimal drag characteristics of hypersonic aircraf
The present work takes origin from studies carried out at the Department of Aerospace Engineering of...
It has been shown that the problem of finding minimum drag configuration in hypersonic flow can be ...
A unified treatment is given to the problem of finding minimum total drag bodies-both two-dimensiona...
Variational calculus methods for drag reduction of lifting bodies in hypersonic flo
Optimum contours for internaI shapes in Newtonian hypersonic flow with constant and variable skin fr...
A new method was developed to optimize, in terms of aerodynamic wave drag minimization, arbitrary (n...
Control programs and flight paths of a hypersonic vehicle in climb are analyzed. Two approaches to s...
. In this paper, a method based on the optimal control theory for the solution of shape optimization...
This paper presents the classic approach to minimum drag shape body problem, moving at hypersonic sp...
By use of an approximate equation for the wave drag of slender bodies of revolution in a supersonic ...
Abstract. The efficient direct optimization method for supersonic aircraft design is presented. The ...
A theoretical investigation is made of the airfoil profile for minimum pressure drag at zero lift in...
Analytical solutions for variational problems on configurations of threedimensional (3D) bodies with...
Abstract. The problem on the configuration with maximum lift-to-drag ratio in supersonic gas flow is...
Optimum body length and volume design for minimal drag characteristics of hypersonic aircraf
The present work takes origin from studies carried out at the Department of Aerospace Engineering of...
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