Symmetrical, equilibrium flow past a blunt body at superorbital re-entry speeds.
Symmetrical equilibrium flow past blunt body at superorbital reentry conditions calculated by integrating motion equations across shock layer
FLOW STABILITY↗
Engineering topics
Publications and source records attributed to Byron, S. R..
Symmetrical equilibrium flow past blunt body at superorbital reentry conditions calculated by integrating motion equations across shock layer
Theoretical prediction of state of gas in flow field surrounding Apollo type vehicle in reentry at hypersonic speeds