Calculated radio attenuation due to plasma sheath of hypersonic blunt-nosed cone
Calculated radio attenuation due to plasma sheath on hypersonic blunt-nosed cone
BLUNT BODY↗
Engineering topics
Huber, P. W.
Publications and source records attributed to Huber, P. W..
Hypersonic shock-heated flow parameters for velocities to 46,000 feet per second and altitudes to 323,000 feet
Real air hypersonic shock-heated flow parameters at high speeds and high altitudes
SHOCK HEATING↗
Radio transmission through the plasma sheath around a lifting reentry vehicle
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Ellis, M. C., Jr.↗