Add to ORKGCalculation of shock inclination angle and surface pressure coefficient in vertical plane of symmetry of bodies at angle of attack related to delta wing-body space shuttle orbite
An engineering-type procedure is presented for computing normal-force, axial-force, and pitching-mom...
An analysis of the unsteady aerodynamics of space shuttle vehicles was performed. The results show t...
Modification of mathematical approach to general body problem for investigating direct shock wave pr...
Methods for prediction of centerline shock layer thickness and pressure distribution on delta wing b...
Pressure distributions on flat plate delta wing swept 65 deg at hypersonic speeds at angles of attac...
An experimental investigation was conducted on space shuttle type, body-wing configurations. The pur...
The equations which govern the viscous shock-layer flow are presented and the method by which the eq...
Pitot pressure distributions of the flow field of a 0.0075-scale model of a typical delta wing shutt...
An experimental investigation of inviscid real-gas effects on the pressure distribution along the Sp...
Effects of angle of attack and bluntness on shock layer properties of cones at supersonic speed
A method is presented for determining shock envelopes and pressure distributions for two-dimensional...
A general method developed for the analysis of inviscid hypersonic shock layers is discussed for app...
Linearized characteristics method, and equivalent body method for predicting flow field about axisym...
Aerodynamic heating distributions on model of space shuttle delta wing orbiter with twin wing-tip ve...
Spatial distribution of radiant heat in reentry vehicle hypersonic shock layers at angle of attac
An engineering-type procedure is presented for computing normal-force, axial-force, and pitching-mom...
An analysis of the unsteady aerodynamics of space shuttle vehicles was performed. The results show t...
Modification of mathematical approach to general body problem for investigating direct shock wave pr...
Methods for prediction of centerline shock layer thickness and pressure distribution on delta wing b...
Pressure distributions on flat plate delta wing swept 65 deg at hypersonic speeds at angles of attac...
An experimental investigation was conducted on space shuttle type, body-wing configurations. The pur...
The equations which govern the viscous shock-layer flow are presented and the method by which the eq...
Pitot pressure distributions of the flow field of a 0.0075-scale model of a typical delta wing shutt...
An experimental investigation of inviscid real-gas effects on the pressure distribution along the Sp...
Effects of angle of attack and bluntness on shock layer properties of cones at supersonic speed
A method is presented for determining shock envelopes and pressure distributions for two-dimensional...
A general method developed for the analysis of inviscid hypersonic shock layers is discussed for app...
Linearized characteristics method, and equivalent body method for predicting flow field about axisym...
Aerodynamic heating distributions on model of space shuttle delta wing orbiter with twin wing-tip ve...
Spatial distribution of radiant heat in reentry vehicle hypersonic shock layers at angle of attac
An engineering-type procedure is presented for computing normal-force, axial-force, and pitching-mom...
An analysis of the unsteady aerodynamics of space shuttle vehicles was performed. The results show t...
Modification of mathematical approach to general body problem for investigating direct shock wave pr...