Add to ORKGNumerical calculations were made of flow fields generated by various aerodynamic configurations. Dat...
A user's manual is presented for a program that calculates the supersonic flow on the windward side ...
The laminar boundary-layer flow about a circular cone at large angles of a t tack t o a supersonic s...
Analysis of supersonic conical flow and solutions for subsonic region on compression side of delta w...
Points treated in this report are: homogeneous flows, the general study of conical flows with infini...
A fully conservative numerical method for the computation of steady inviscid supersonic flow about g...
Method of lines technique for computing flow field about conical configurations at incidence in supe...
Supersonic linearized conical-flow theory is used to determine the flow over slender pointed cones h...
Steady, inviscid, supersonic flow past conical wings is studied within the context of irrotational, ...
Two complementary procedures were developed to calculate the viscous supersonic flow over conical sh...
The inverse method, with the shock wave prescribed to be an elliptic cone at a finite angle of incid...
The problem of inviscid, steady transonic conical flow, formulated in terms of the small disturbance...
Direct calculation method for supersonic inviscid flow around axisymmetric blunt body with conically...
The method of superposition of linearized conical flows has been applied to the calculation of the a...
A user's manual for a computer program which calculates the supersonic flow about circular, elliptic...
Numerical calculations were made of flow fields generated by various aerodynamic configurations. Dat...
A user's manual is presented for a program that calculates the supersonic flow on the windward side ...
The laminar boundary-layer flow about a circular cone at large angles of a t tack t o a supersonic s...
Analysis of supersonic conical flow and solutions for subsonic region on compression side of delta w...
Points treated in this report are: homogeneous flows, the general study of conical flows with infini...
A fully conservative numerical method for the computation of steady inviscid supersonic flow about g...
Method of lines technique for computing flow field about conical configurations at incidence in supe...
Supersonic linearized conical-flow theory is used to determine the flow over slender pointed cones h...
Steady, inviscid, supersonic flow past conical wings is studied within the context of irrotational, ...
Two complementary procedures were developed to calculate the viscous supersonic flow over conical sh...
The inverse method, with the shock wave prescribed to be an elliptic cone at a finite angle of incid...
The problem of inviscid, steady transonic conical flow, formulated in terms of the small disturbance...
Direct calculation method for supersonic inviscid flow around axisymmetric blunt body with conically...
The method of superposition of linearized conical flows has been applied to the calculation of the a...
A user's manual for a computer program which calculates the supersonic flow about circular, elliptic...
Numerical calculations were made of flow fields generated by various aerodynamic configurations. Dat...
A user's manual is presented for a program that calculates the supersonic flow on the windward side ...
The laminar boundary-layer flow about a circular cone at large angles of a t tack t o a supersonic s...