Add to ORKGThe generalized shock-expansion method is applied to obtain solutions to the flow field about pointed bodies of revolution at high supersonic airspeeds and small angles of attack. Simple explicit expressions are obtained for the surface Mach numbers and surface pressures in the special case of slender bodies. In the case of inclined cones, algebraic solutions are obtained defining the entire flow field. Experimental pressure-distribution data for cones and ogives at Mach numbers from 3 to 5 are included. (author
The paper discusses the development and testing of shock-expansion tool for 2-D and axisymmetric sup...
The simplified solution for the pressure distribution of slender inclined bodies of revolution is de...
A general method for the analysis of the inviscid asymmetric hypersonic flow fields enveloping smoot...
The generalized shock-expansion method is applied to obtain solutions to the flow field about pointe...
A second-order shock-expansion method applicable to bodies of revolution is developed by the use of ...
A procedure for calculating three-dimensional steady and nonsteady supersonic flows with the method ...
linearized theory, second-order theory, tangent-cone method, conical-shock-expansiontheory, and Newt...
Pressure distributions and force characteristics have been determined for a body of revolution consi...
The theory developed by G.B. Whitham (Communications on Pure and Applied Mathematics, August 1952) f...
An approximate method is presented for the calculation of the external lift, moment, and pressure dr...
The method of characteristics has been applied for the determination of the supersonic-flow properti...
An experimental investigation was conducted in the GALCIT hypersonic blow-down tunnel to determine ...
Solving exact gas dynamic equations for supersonic flows far from axis of slender lifting bodie
Development of near-field method for determining supersonic flow properties about bodies of revoluti...
The aerodynamic stability derivatives due to pitching velocity and vertical acceleration are derived...
The paper discusses the development and testing of shock-expansion tool for 2-D and axisymmetric sup...
The simplified solution for the pressure distribution of slender inclined bodies of revolution is de...
A general method for the analysis of the inviscid asymmetric hypersonic flow fields enveloping smoot...
The generalized shock-expansion method is applied to obtain solutions to the flow field about pointe...
A second-order shock-expansion method applicable to bodies of revolution is developed by the use of ...
A procedure for calculating three-dimensional steady and nonsteady supersonic flows with the method ...
linearized theory, second-order theory, tangent-cone method, conical-shock-expansiontheory, and Newt...
Pressure distributions and force characteristics have been determined for a body of revolution consi...
The theory developed by G.B. Whitham (Communications on Pure and Applied Mathematics, August 1952) f...
An approximate method is presented for the calculation of the external lift, moment, and pressure dr...
The method of characteristics has been applied for the determination of the supersonic-flow properti...
An experimental investigation was conducted in the GALCIT hypersonic blow-down tunnel to determine ...
Solving exact gas dynamic equations for supersonic flows far from axis of slender lifting bodie
Development of near-field method for determining supersonic flow properties about bodies of revoluti...
The aerodynamic stability derivatives due to pitching velocity and vertical acceleration are derived...
The paper discusses the development and testing of shock-expansion tool for 2-D and axisymmetric sup...
The simplified solution for the pressure distribution of slender inclined bodies of revolution is de...
A general method for the analysis of the inviscid asymmetric hypersonic flow fields enveloping smoot...