To study shock layer radiative phenomena, experimental studies of equilibrium radiative heating during re-entry were undertaken at Ohio State University; using arc-driven shock-tube facility, measurements of total stagnation-point equilibrium radiative heat flux in wavelength region of 0.17 to 6.0 Μ were carried out over range of simulated flight velocities from 26,000 to 52,000 fps and at simulated altitudes from 100,000 to 170,000 ft; experimental techniques applied, and results obtained are reported.
Shock-tube studies of equilibrium air radiation
AIAA J
AIAA Journal ; 3 , n 6
1965
8 pages
Aufsatz (Zeitschrift)
Englisch
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Shock-tube studies of equilibrium air radiation
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