Add to ORKGPerturbation solution to blunt body stagnation region flow of radiating gas with radiation heat transfe
Stagnation point radiative heating rates for manned vehicles entering the earth's atmosphere at para...
Effect of radiative heat transfer in low Reynolds number hypersonic flow about blunt bod
An approximate theory is developed for predicting the rate of heat transfer to the stagnation region...
Coupling between inviscid and viscid flows in hypersonic stagnation region investigated at high flig...
Prepared at Langley Research Center."January 1969"--Cover.Includes bibliographical references (p. 27...
The recent resurgence of interest in blunt-body atmospheric entry for applications such as aeroassis...
The laminar compressible boundary layer in the two-dimensional and axisymmetric stagnation regions h...
A closed-form equation is derived for stagnation point reentry radiative heat transfer accounting fo...
Radiative and convective heat transfer about two blunt bodies traveling at hypersonic speeds at zero...
Stagnation point convective heat transfer for blunt body moving at hypersonic spee
A mathematical model of the aerothermochemical environment along the stagnation line of a planetary ...
Finite difference techniques used in numerical solutions for inviscid radiating shock layers around ...
A viscous shock-layer analysis is for calculating high energy equilibrium flow fields about blunt ax...
Two-dimensional analysis of radiant heat transfer to absorbing gases with flow and conductio
Solution for shock layer energy equation with mass and convective heat transfer at hypersonic spee
Stagnation point radiative heating rates for manned vehicles entering the earth's atmosphere at para...
Effect of radiative heat transfer in low Reynolds number hypersonic flow about blunt bod
An approximate theory is developed for predicting the rate of heat transfer to the stagnation region...
Coupling between inviscid and viscid flows in hypersonic stagnation region investigated at high flig...
Prepared at Langley Research Center."January 1969"--Cover.Includes bibliographical references (p. 27...
The recent resurgence of interest in blunt-body atmospheric entry for applications such as aeroassis...
The laminar compressible boundary layer in the two-dimensional and axisymmetric stagnation regions h...
A closed-form equation is derived for stagnation point reentry radiative heat transfer accounting fo...
Radiative and convective heat transfer about two blunt bodies traveling at hypersonic speeds at zero...
Stagnation point convective heat transfer for blunt body moving at hypersonic spee
A mathematical model of the aerothermochemical environment along the stagnation line of a planetary ...
Finite difference techniques used in numerical solutions for inviscid radiating shock layers around ...
A viscous shock-layer analysis is for calculating high energy equilibrium flow fields about blunt ax...
Two-dimensional analysis of radiant heat transfer to absorbing gases with flow and conductio
Solution for shock layer energy equation with mass and convective heat transfer at hypersonic spee
Stagnation point radiative heating rates for manned vehicles entering the earth's atmosphere at para...
Effect of radiative heat transfer in low Reynolds number hypersonic flow about blunt bod
An approximate theory is developed for predicting the rate of heat transfer to the stagnation region...