Add to ORKGRelationship of shock standoff distance, at sonic and stagnation points, to body geometry of blunt bodies at zero angle of attac
The theory developed by G.B. Whitham (Communications on Pure and Applied Mathematics, August 1952) f...
Curved shocks that are locally oriented normal to the direction of the pre-shock flow vector appear ...
Wind tunnel measurements on effect of slender body shape on sonic boom pressure distribution
A method is presented for determining shock envelopes and pressure distributions for two-dimensional...
A method for determining shock-wave shapes, stagnation-point location, and flow-field properties for...
Linearized characteristics method, and equivalent body method for predicting flow field about axisym...
A systematic analysis of Newtonian flow past an axi-symmetrical blunt body is developed by expanding...
Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack f...
Pressure distributions, aerodynamic coefficients, and shock shapes were measured on blunt bodies of ...
In this paper it is addressed the prediction of form and location of detached shock waves ahead of t...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
Direct calculation method for supersonic inviscid flow around axisymmetric blunt body with conically...
Numerical analysis of free flow fields around axisymmetric blunt bodies in supersonic fligh
An approximate method, based on a simplified form of the con-tinuity relation, is developed to predi...
Pressure distributions and shock shapes for a series of cylindrical afterbodies having nose fineness...
The theory developed by G.B. Whitham (Communications on Pure and Applied Mathematics, August 1952) f...
Curved shocks that are locally oriented normal to the direction of the pre-shock flow vector appear ...
Wind tunnel measurements on effect of slender body shape on sonic boom pressure distribution
A method is presented for determining shock envelopes and pressure distributions for two-dimensional...
A method for determining shock-wave shapes, stagnation-point location, and flow-field properties for...
Linearized characteristics method, and equivalent body method for predicting flow field about axisym...
A systematic analysis of Newtonian flow past an axi-symmetrical blunt body is developed by expanding...
Pressure distributions for blunt body wind tunnel models at supersonic speeds and angles of attack f...
Pressure distributions, aerodynamic coefficients, and shock shapes were measured on blunt bodies of ...
In this paper it is addressed the prediction of form and location of detached shock waves ahead of t...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
Direct calculation method for supersonic inviscid flow around axisymmetric blunt body with conically...
Numerical analysis of free flow fields around axisymmetric blunt bodies in supersonic fligh
An approximate method, based on a simplified form of the con-tinuity relation, is developed to predi...
Pressure distributions and shock shapes for a series of cylindrical afterbodies having nose fineness...
The theory developed by G.B. Whitham (Communications on Pure and Applied Mathematics, August 1952) f...
Curved shocks that are locally oriented normal to the direction of the pre-shock flow vector appear ...
Wind tunnel measurements on effect of slender body shape on sonic boom pressure distribution