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Onset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel / Robert M. Hall.

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Series Information

NASA technical paper

Record details

  • Physical Description: 1 online resource (69 pages) : illustrations.
  • Publisher: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office, April 1979.

Content descriptions

General Note:
Title from title screen (viewed on Aug. 10, 2016).
"April 1979."
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Bibliography, etc. Note:
Includes bibliographical references (pages 22-23).
Type of Report and Period Covered Note:
Technical paper.
Funding Information Note:
National Aeronautics and Space Administration 505-06-43-08
L-12581
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074 . ‡a0830-H-15 (online)
0860 . ‡aNAS 1.60:1385
1001 . ‡aHall, Robert M., ‡eauthor. ‡0(EG-IN)1184168
24510. ‡aOnset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel / ‡cRobert M. Hall.
260 . ‡a[Washington, D.C.] : ‡bNational Aeronautics and Space Administration, Scientific and Technical Information Office, ‡cApril 1979.
300 . ‡a1 online resource (69 pages) : ‡billustrations.
336 . ‡atext ‡btxt ‡2rdacontent
337 . ‡acomputer ‡bc ‡2rdamedia
338 . ‡aonline resource ‡bcr ‡2rdacarrier
4901 . ‡aNASA technical paper ; ‡v1385
500 . ‡aTitle from title screen (viewed on Aug. 10, 2016).
500 . ‡a"April 1979."
500 . ‡a"Performing Organization: NASA Langley Research Center"--Report documentation page.
504 . ‡aIncludes bibliographical references (pages 22-23).
513 . ‡aTechnical paper.
536 . ‡aNational Aeronautics and Space Administration ‡h505-06-43-08
536 . ‡dL-12581
7102 . ‡aLangley Research Center. ‡0(EG-IN)1118311
7101 . ‡aUnited States. ‡bNational Aeronautics and Space Administration. ‡bScientific and Technical Information Office, ‡eissuing body. ‡0(EG-IN)980802
77608. ‡iPrint version: ‡aHall, Robert M. ‡tOnset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel ‡w(OCoLC)7261120
77608. ‡iMicrofiche version: ‡aHall, Robert M. ‡tOnset of condensation effects with an NACA 0012-64 airfoil tested in the Langley 0.3-meter transonic cryogenic tunnel ‡w(OCoLC)711544672
830 0. ‡aNASA technical paper ‡0(DLC)1179746
85640. ‡uhttp://purl.fdlp.gov/GPO/gpo70962 ‡9STLIB-IND
949 . ‡hONLINE
901 . ‡aocn784798060 ‡bOCoLC ‡c20810583 ‡tbiblio ‡sGPO - Government Documents

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