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A Radiant Heater to Simulate Aerodynamic Heating in a Wind TunnelA recently developed radiant-heating test technique for simulation of aerodynamic heating in wind tunnel is describes. The heating device, which utilized quartz-tube lamps, was operated successfully while exposed directly to a supersonic airstream. Tests were made on a calibration panel, and experimental temperature and pressure data are presented. Results indicate that initial heating rates of about 26 Btu/(sq ft) (sec) are obtainable at a distance of 12 inches from the heater. Further applications of the basic design are discussed briefly.
Document ID
20040047051
Acquisition Source
Headquarters
Document Type
Other - NASA Technical Note (TN)
Authors
Trussell, Donald H.
(NASA Langley Research Center Hampton, VA, United States)
Weidman, Deene J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 21, 2013
Publication Date
November 1, 1960
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
L-917
NASA/TN-D-530
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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