Item Details

Studies of Condensation Effects on Airfoil Testing in the Langley 0.3-Meter Transonic Cryogenic Tunnel

Robert M. Hall
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
Language
English
Series
NASA Technical Paper
SuDoc Number
NAS 1.60:2509
Description
31 p. : ill. ; 28 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • "January 1986"--Cover.
  • Includes bibliographical references (p. 11-12).
Series Statement
NASA technical paper ; 2509
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

  • LEADER 01551nam a2200409Ia 4500
    001 011425335
    003 MiAaHDL
    005 20141013010000.0
    006 m d
    007 cr bn ---auaua
    008 970422s1986 dcua b f000 0 eng d
    035
      
      
    a| sdr-uiuc6361459
    035
      
      
    a| (OCoLC)36781726
    040
      
      
    a| ABC c| ABC
    049
      
      
    a| UIUU
    086
    0
      
    a| NAS 1.60:2509
    090
      
      
    a| TL521.3 b| .N18 no. 2509
    100
    1
      
    a| Hall, Robert M.
    245
    1
    0
    a| Studies of condensation effects on airfoil testing in the Langley 0.3-meter transonic cryogenic tunnel / c| Robert M. Hall.
    260
      
      
    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,
    300
      
      
    a| 31 p. : b| ill. ; c| 28 cm.
    490
      
    0
    a| NASA technical paper ; v| 2509
    500
      
      
    a| Prepared at Langley Research Center.
    500
      
      
    a| "January 1986"--Cover.
    504
      
      
    a| Includes bibliographical references (p. 11-12).
    538
      
      
    a| Mode of access: Internet.
    650
      
    0
    a| Consensation.
    650
      
    0
    a| Aerofoils x| Testing.
    650
      
    0
    a| Wind tunnels.
    710
    2
      
    a| Langley Research Center.
    974
      
      
    b| UIU c| UIUC d| 20161008 s| google u| uiug.30112106614479 y| 1986 r| pd q| bib

Access online

Google Preview