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Title
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A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel /
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Format
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online resource
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Internet Access
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https://purl.fdlp.gov/GPO/gpo71172
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Author
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Lawing, Pierce L., author.
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Published
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[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
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SuDoc Number
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NAS 1.60:1752
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Item Number
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0830-H-15 (online)
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Description
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1 online resource (18 pages) : illustrations.
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Content Type
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text
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Series
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(NASA technical paper ; 1752.)
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General Note
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Title from title screen (viewed on Aug. 17, 2016).
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"November 1980."
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"Performing Organization: NASA Langley Research Center"--Report documentation page.
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Bibliography
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Includes bibliographical references (page 11).
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Added Entry
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Adcock, Jerry B., author.
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Ladson, Charles L., author.
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Added Entry
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Langley Research Center.
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United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
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Linking Field
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Print 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
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Microfiche 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
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URL
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http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19810001497.pdf
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Holdings
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All items
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OCLC Number
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(OCoLC)761455916
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CGP Record Link
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https://catalog.gpo.gov:443/F/?func=direct&doc_number=000991683&local_base=GPO01PUB
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System Number
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000991683
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