Measurements of radiation from the flow fields of bodies flying at speeds up to 13.4 kilometers per second.
Radiation emission from shock layer about small models flying at velocities up to 13.4 km/sec
AIR↗
Engineering topics
Canning, T. N.
Publications and source records attributed to Canning, T. N..
Physics of hypervelocity flight as it affects the design of re-entry vehicles.
Characteristics of air at high temperatures for consideration in design of reentering space vehicles
AIR↗
THE PHYSICS OF HYPERVELOCITY FLIGHT AS IT AFFECTS THE DESIGN OF REENTRY VEHICLES
Characteristics of air at high temperatures for consideration in the design of reentering space vehicles
AIR↗
MEASUREMENTS OF RADIATION FROM THE FLOW FIELDS OF BODIES FLYING AT SPEEDS UP TO 13.4 KILOMETERS PER SECOND
Measurements of radiation from the flow fields of bodies flying at speeds up to 13.4 km per second
RADIATION↗
MEASUREMENTS OF THERMAL RADIATION OF AIR FROM THE STAGNATION REGION OF BLUNT BODIES TRAVELING AT VELOCITIES UP TO 31,000 FEET PER SECOND
Thermal radiation of air from stagnation region of blunt bodies at hypersonic speed
HYPERSONIC SPEED↗
Measurements of radiation from air and carbon dioxide
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Canning, T. N.↗