Item Details

Pressure Distributions From High Reynolds Number Tests of a NASA SC(3)-0712(B) Airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

William G. Johnson, Jr., Acquilla S. Hill, and Otto Eichmann
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
Language
English
Series
NASA Technical Memorandum
Description
406 p. : ill. ; 28 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • Bibliography: p. 390.
Series Statement
NASA technical memorandum ; 86370
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Pressure distributions from high Reynolds number tests of a NASA SC(3)-0712(B) airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel / c| William G. Johnson, Jr., Acquilla S. Hill, and Otto Eichmann.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration, Scientific and Technical Information Branch ; a| Springfield, Va. : b| For sale by the National Technical Information Service, c| 1985.
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    a| NASA technical memorandum ; v| 86370
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    a| Mode of access: Internet.
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    a| Transonic wind tunnels.
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    a| Low temperature research.
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    a| Reynolds number.
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    a| Aerodynamics, Transonic.
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