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Title   A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel /
Format   online resource
Internet Access   https://purl.fdlp.gov/GPO/gpo71172  
Author   LinkLawing, Pierce L., author.
Published   [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
 
SuDoc Number   LinkNAS 1.60:1752
Item Number   Link0830-H-15 (online)
Description   1 online resource (18 pages) :  illustrations.
Content Type   text
Series   Link(NASA technical paper ; 1752.)
General Note   Title from title screen (viewed on Aug. 17, 2016).
  "November 1980."
  "Performing Organization: NASA Langley Research Center"--Report documentation page.
Bibliography   Includes bibliographical references (page 11).
Added Entry   LinkAdcock, Jerry B., author.
  LinkLadson, Charles L., author.
Added Entry   LinkLangley Research Center.
  LinkUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Linking Field   LinkPrint version: Lawing, Pierce L. Fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel (OCoLC)7437680
  LinkMicrofiche version: Lawing, Pierce L. Fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel (OCoLC)711544796
URL   http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19810001497.pdf  
 
Holdings   All items
 
OCLC Number   (OCoLC)761455916
CGP Record Link   https://catalog.gpo.gov:443/F/?func=direct&doc_number=000991683&local_base=GPO01PUB
System Number   000991683


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