Accurate definition of severity of planetary entry problem has been made difficult by complexity of performing experiments in this environment; study applies new technique to heat-transfer measurements in shock tube at simulated flight velocities up to 50,000 fps using IR heat-transfer gage which has been adapted to this experiment; difficulties of adapting gage to test requirements are described, as well as calibration of IR cell output and response time characteristics of measuring system.
Heat-transfer measurements in partially ionized air
AIAA J
AIAA Journal ; 3 , n 9
1965
9 pages
Article (Journal)
English
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Heat-Transfer Measurements in Partially Ionized Air
AIAA | 1965
|Heat transfer measurements in partially ionized gases
TIBKAT | 1965
|