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Test program on thin-walled tubes with zero thermal gradient Final reportTest program on deflection characteristics of thin walled stem tubes perforated with random spiral hole pattern to produce equal absorption of radiant power on front and rear surface
Document ID
19660024282
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Flood, J. (De Havilland Aircraft Co. of Canada Ltd. Malton Ontario, Canada)
Kerr, H. S. (De Havilland Aircraft Co. of Canada Ltd. Malton Ontario, Canada)
Spencer, R. (De Havilland Aircraft Co. of Canada Ltd. Malton Ontario, Canada)
Date Acquired
August 3, 2013
Publication Date
January 1, 1966
Subject Category
Structural Mechanics
Report/Patent Number
DHC-SP-R.168-2
NASA-CR-76917
Report Number: DHC-SP-R.168-2
Report Number: NASA-CR-76917
Accession Number
66N33572
Funding Number(s)
CONTRACT_GRANT: NAS5-9572
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TUBE
THERMAL ABSORPTION
DEFLECTION
TEST PROGRAM
THIN WALL
RADIANT HEATING

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