Results of solving the Navier-Stokes equations for chemically nonequilibrium, merged stagnation shock layers on spheres and two-dimensional cylinders are presented. The effects of wall catalysis and slip are also examined. The thin shock layer assumption is not made, and the thick viscous shock is allowed to develop within the computational domain. The results show good comparison with existing data. Due to the more pronounced merging of shock layer and boundary layer for the sphere, the heating rates for spheres become higher than those for cylinders as the altitude is increased
The backward Euler scheme was used to solve a large system of inviscid flow and chemical rate equati...
The physical phenomena within supersonic flows that sustain chemical reactions are investigated. An ...
This dissertation presents a detailed, computational study quantifying the effects of nonequilibrium...
Numerical solutions are presented for the viscous shocklayer equations where the chemistry is treate...
A new procedure seeks to combine the thin-layer Navier-Stokes solver LAURA with the parabolized Navi...
The viscous-shock-layer equations for hypersonic laminar and turbulent flows of radiating or nonradi...
Results are obtained for cylindrical leading edges of proposed transatmospheric vehicles by employin...
The nonequilibrium chemical reaction of dissociation and recombination is studied theoretically for ...
The flow field in and around the nozzle afterbody section of a hypersonic vehicle was computationall...
This paper presents a nonequilibrium flow solver, implementation of the algorithm on unstructured me...
The nature of the nonequilibrium flow of dissociating gases over spheres was investigated experiment...
The equations which govern the viscous shock-layer flow are presented and the method by which the eq...
A mathematical model of the aerothermochemical environment along the stagnation line of a planetary ...
An analysis of nonequilibrium-dissociated stagnation point flow on highly cooled blunt bodies in a h...
Thermochemical effects of foreign planetary atmospheres upon laminar heat transfer in hypersonic sta...
The backward Euler scheme was used to solve a large system of inviscid flow and chemical rate equati...
The physical phenomena within supersonic flows that sustain chemical reactions are investigated. An ...
This dissertation presents a detailed, computational study quantifying the effects of nonequilibrium...
Numerical solutions are presented for the viscous shocklayer equations where the chemistry is treate...
A new procedure seeks to combine the thin-layer Navier-Stokes solver LAURA with the parabolized Navi...
The viscous-shock-layer equations for hypersonic laminar and turbulent flows of radiating or nonradi...
Results are obtained for cylindrical leading edges of proposed transatmospheric vehicles by employin...
The nonequilibrium chemical reaction of dissociation and recombination is studied theoretically for ...
The flow field in and around the nozzle afterbody section of a hypersonic vehicle was computationall...
This paper presents a nonequilibrium flow solver, implementation of the algorithm on unstructured me...
The nature of the nonequilibrium flow of dissociating gases over spheres was investigated experiment...
The equations which govern the viscous shock-layer flow are presented and the method by which the eq...
A mathematical model of the aerothermochemical environment along the stagnation line of a planetary ...
An analysis of nonequilibrium-dissociated stagnation point flow on highly cooled blunt bodies in a h...
Thermochemical effects of foreign planetary atmospheres upon laminar heat transfer in hypersonic sta...
The backward Euler scheme was used to solve a large system of inviscid flow and chemical rate equati...
The physical phenomena within supersonic flows that sustain chemical reactions are investigated. An ...
This dissertation presents a detailed, computational study quantifying the effects of nonequilibrium...