The Resource A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel, Pierce L. Lawing, Jerry B. Adcock, and Charles L. Ladson

A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel, Pierce L. Lawing, Jerry B. Adcock, and Charles L. Ladson

Label
A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel
Title
A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel
Statement of responsibility
Pierce L. Lawing, Jerry B. Adcock, and Charles L. Ladson
Creator
Contributor
Author
Issuing body
Subject
Language
eng
Member of
Cataloging source
OCLCE
http://library.link/vocab/creatorName
Lawing, Pierce L
Funding information
National Aeronautics and Space Administration
Government publication
federal national government publication
Illustrations
illustrations
Index
no index present
Literary form
non fiction
Nature of contents
  • dictionaries
  • bibliography
  • technical reports
http://library.link/vocab/relatedWorkOrContributorName
  • Adcock, Jerry B.
  • Ladson, Charles L.
  • Langley Research Center
  • United States
Series statement
NASA technical paper
Series volume
1752
http://library.link/vocab/subjectName
  • Mach number
  • Pressure measurement
  • Reynolds number
  • Transonic wind tunnels
  • Wind tunnel calibration
Type of report
Technical paper.
Label
A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel, Pierce L. Lawing, Jerry B. Adcock, and Charles L. Ladson
Link
http://purl.fdlp.gov/GPO/gpo71172
Instantiates
Publication
Note
  • Title from title screen (viewed on Aug. 17, 2016)
  • "November 1980."
  • "Performing Organization: NASA Langley Research Center"--Report documentation page
  • Available online
Bibliography note
Includes bibliographical references (page 11)
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
Control code
ocn761455916
Dimensions
unknown
Extent
1 online resource (18 pages)
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
c
Other physical details
illustrations.
Specific material designation
remote
Label
A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel, Pierce L. Lawing, Jerry B. Adcock, and Charles L. Ladson
Link
http://purl.fdlp.gov/GPO/gpo71172
Publication
Note
  • Title from title screen (viewed on Aug. 17, 2016)
  • "November 1980."
  • "Performing Organization: NASA Langley Research Center"--Report documentation page
  • Available online
Bibliography note
Includes bibliographical references (page 11)
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
Control code
ocn761455916
Dimensions
unknown
Extent
1 online resource (18 pages)
Form of item
online
Media category
computer
Media MARC source
rdamedia
Media type code
c
Other physical details
illustrations.
Specific material designation
remote

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