Experimental study of radiation cooling effects in a hypervelocity shock layer.
Radiative energy emission by blunt vehicle shock layer under severe entry conditions, discussing flow properties and radiative transfer coupling
Engineering topics
Publications and source records attributed to Gruszczynski, J. S..
Radiative energy emission by blunt vehicle shock layer under severe entry conditions, discussing flow properties and radiative transfer coupling
Equilibrium air total radiation mechanism, vacuum UV radiation and relation to hypervelocity entry studied, using shock tube blunt model test flow
High-temperature gas radiance in simulated planetary atmosphere at various entry velocities
Equilibrium air total radiation mechanism, vacuum UV radiation and relation to hypervelocity entry studied, using shock tube blunt model test flow
Windowless total radiation gauge for shock tube measurements of high temperature gas radiance
Equilibrium radiation in air and gas mixtures assumed to represent near planet atmospheres
Techniques for measurement of equilibrium and non equilibrium radiance of high temperature gases in electric driven shock tube
Experimental study of equilibrium air total radiation
Shock tube instrumentation to study convective and radiative heat transfer of hot gases simulating hypervelocity reentry
Shock tube instrumentation methods for convective heat transfer study and radiative properties of high temperature gas at conditions simulating hypervelocity entry
Hypervelocity heat transfer studies in simulated planetary atmospheres
Laboratory simulation of hypervelocity heat transfer problem during planetary entry
Heat transfer problems with a ballistic vehicle entering into the atmospheres of near planets at hypervelocity entry conditions
Heat transfer on hypersonic vehicle entering a planetary atmosphere