A review is given of computations for a series of nominally 2-D laminar viscous-inviscid interactions. Comparisons were made with detailed experimental shock tunnel results. The shock wave boundary layer interactions considered were induced by a compression ramp in one case and by an externally generated incident shock in the second case. In general, good agreement was reached between the grid refined calculations and experiment for the incipient and small separation conditions. For the highly separated flow, 3-D calculations which included the finite span effects of the experiment were required in order to obtain agreement with the data
The convective heat transfer distribution for space shuttle configurations is discussed. The viscous...
The proper design of engine nacelle installations for supersonic aircraft depends on a sophisticated...
The interaction of an impinging shock with the bow-shock generated by a blunt geometry is examined n...
An efficient time-splitting, second-order accurate, numerical scheme is used to solve the complete N...
Experimental data on fully laminar and transitional shock-wave/boundary-layer interactions in two-di...
Approximate methods for calculating the surface pressures including the effects of viscous interacti...
This report describes a theoretical and experimental investigation of the properties of attached and...
Experimental studies were conducted to examine the aerothermal characteristics of shock/shock/bounda...
A variety of practical fluid dynamic problems related to the low-speed, high Reynolds number flow ov...
This report presents the results of an investigation of hypersonic laminar boundary-layer/shock-wave...
An assessment is presented for the experimental data on separated flow in shock wave turbulent bound...
Two-dimensional viscous blunt body flows with an impinging shock have been computed using a time-dep...
The effect of shock impingement on the blunt leading edges of the top and sidewall compression type ...
Numerical investigations of laminar shock-wave/boundary-layer interactions (SWBLIs) in hypersonic fl...
A time dependent finite difference method used to calculate blunt body flows with impinging shock is...
The convective heat transfer distribution for space shuttle configurations is discussed. The viscous...
The proper design of engine nacelle installations for supersonic aircraft depends on a sophisticated...
The interaction of an impinging shock with the bow-shock generated by a blunt geometry is examined n...
An efficient time-splitting, second-order accurate, numerical scheme is used to solve the complete N...
Experimental data on fully laminar and transitional shock-wave/boundary-layer interactions in two-di...
Approximate methods for calculating the surface pressures including the effects of viscous interacti...
This report describes a theoretical and experimental investigation of the properties of attached and...
Experimental studies were conducted to examine the aerothermal characteristics of shock/shock/bounda...
A variety of practical fluid dynamic problems related to the low-speed, high Reynolds number flow ov...
This report presents the results of an investigation of hypersonic laminar boundary-layer/shock-wave...
An assessment is presented for the experimental data on separated flow in shock wave turbulent bound...
Two-dimensional viscous blunt body flows with an impinging shock have been computed using a time-dep...
The effect of shock impingement on the blunt leading edges of the top and sidewall compression type ...
Numerical investigations of laminar shock-wave/boundary-layer interactions (SWBLIs) in hypersonic fl...
A time dependent finite difference method used to calculate blunt body flows with impinging shock is...
The convective heat transfer distribution for space shuttle configurations is discussed. The viscous...
The proper design of engine nacelle installations for supersonic aircraft depends on a sophisticated...
The interaction of an impinging shock with the bow-shock generated by a blunt geometry is examined n...