Superorbital entry heat transfer including atomic line radiation and massive blowing
At superorbital reentry velocities radiative heating is the dominant mode of heat transfer to the stagnation region of blunt reentry vehicles. The radiative heat transfer rate at the wall is determined by the temperature profile through the shock layer which depends on the net radiative transport th...
Internet
https://thesis.library.caltech.edu/4513/1/Dirling_rb_1968.pdfDirling, Raymond B. (1969) Superorbital entry heat transfer including atomic line radiation and massive blowing. Engineer's thesis, California Institute of Technology. doi:10.7907/C3KT-S738. https://resolver.caltech.edu/CaltechETD:etd-11112005-161727 <https://resolver.caltech.edu/CaltechETD:etd-11112005-161727>