The Resource Calibration of Mach 2 nozzle blocks with 6% perforated-wall test section, by W.T. Botner, H.R. Spahr, and R.C. Maydew

Calibration of Mach 2 nozzle blocks with 6% perforated-wall test section, by W.T. Botner, H.R. Spahr, and R.C. Maydew

Label
Calibration of Mach 2 nozzle blocks with 6% perforated-wall test section
Title
Calibration of Mach 2 nozzle blocks with 6% perforated-wall test section
Statement of responsibility
by W.T. Botner, H.R. Spahr, and R.C. Maydew
Creator
Contributor
Subject
Language
eng
Summary
"The speed range of the Sandia 12 x 12-inch transonic wind tunnel was recently increased from Mach 1.35 to Mach 2.0 by the installation of interchangeable fixed Mach 2 nozzle blocks."--Page 3
Member of
Action
digitized
Cataloging source
OCLCE
http://bibfra.me/vocab/lite/collectionName
Technical Report Archive & Image Library (TRAIL)
http://library.link/vocab/creatorName
Botner, W. T
Government publication
federal national government publication
Illustrations
illustrations
Index
no index present
Literary form
non fiction
Nature of contents
dictionaries
http://library.link/vocab/relatedWorkOrContributorName
  • Spahr, H. R
  • Maydew, R. C
  • Sandia Corporation
  • U.S. Atomic Energy Commission
Series statement
Sandia Corporation Reprint SCR-129
http://library.link/vocab/subjectName
  • Wind tunnel testing
  • Wind tunnel testing
Label
Calibration of Mach 2 nozzle blocks with 6% perforated-wall test section, by W.T. Botner, H.R. Spahr, and R.C. Maydew
Link
http://catalog.hathitrust.org/api/volumes/oclc/711105013.html
Instantiates
Publication
Note
  • "November 1959."
  • "SCR-129; Aerodynamics; TID-4500 (15th Edition)."
  • "Presented at: Tenth Supersonic Tunnel Association Meeting, Cornell Aeronautical Laboratory, Inc., Buffalo, New York, October 1958"--Page 2 of cover
Antecedent source
file reproduced from original
Carrier category
online resource
Carrier category code
  • cr
Carrier MARC source
rdacarrier
Color
black and white
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent
Dimensions
unknown
Extent
1 online resource (16 pages)
Form of item
online
Level of compression
  • lossless
  • lossy
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations.
Reformatting quality
  • preservation
  • access
Reproduction note
Electronic reproduction.
Specific material designation
remote
System control number
  • (OCoLC)937432530
  • (OCoLC)ocn937432530
System details
Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.
Label
Calibration of Mach 2 nozzle blocks with 6% perforated-wall test section, by W.T. Botner, H.R. Spahr, and R.C. Maydew
Link
http://catalog.hathitrust.org/api/volumes/oclc/711105013.html
Publication
Note
  • "November 1959."
  • "SCR-129; Aerodynamics; TID-4500 (15th Edition)."
  • "Presented at: Tenth Supersonic Tunnel Association Meeting, Cornell Aeronautical Laboratory, Inc., Buffalo, New York, October 1958"--Page 2 of cover
Antecedent source
file reproduced from original
Carrier category
online resource
Carrier category code
  • cr
Carrier MARC source
rdacarrier
Color
black and white
Content category
text
Content type code
  • txt
Content type MARC source
rdacontent
Dimensions
unknown
Extent
1 online resource (16 pages)
Form of item
online
Level of compression
  • lossless
  • lossy
Media category
computer
Media MARC source
rdamedia
Media type code
  • c
Other physical details
illustrations.
Reformatting quality
  • preservation
  • access
Reproduction note
Electronic reproduction.
Specific material designation
remote
System control number
  • (OCoLC)937432530
  • (OCoLC)ocn937432530
System details
Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.

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