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Aerodynamic facilitiesHypersonic shock tunnel and free piston shock tube studies of sixty degree half-angle cones to determine validity of theories of laminar convective heat transfer in planetary gases
Document ID
19680027934
Acquisition Source
Legacy CDMS
Document Type
Other
Date Acquired
August 4, 2013
Publication Date
June 30, 1968
Publication Information
Publication: SPACE PROGRAMS SUM. NO. 37-51, VOL. 3 30 JUN. 1968
Subject Category
Thermodynamics And Combustion
Accession Number
68N37406
Distribution Limits
Public
Copyright
Public Use Permitted.
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