Item Details

Experimental and Numerical Investigation of Boundary-Layer Development and Transition on the Walls of a Mach 5 Nozzle

William D. Harvey, Aubrey M. Cary, Jr., and Julius E. Harris
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975.
Language
English
Series
NASA Technical Note
Description
86 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • Cover title.
  • Includes bibliographical references (p. 23-25).
Series Statement
NASA technical note ; NASA TN D-7976
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

  • LEADER 01748cam a2200457Ia 4500
    001 011443432
    003 MiAaHDL
    005 20141009010000.0
    006 m d
    007 cr bn ---auaua
    008 940405s1975 dcua b f000 0 eng d
    035
      
      
    a| sdr-uiuc6398541
    035
      
      
    a| (OCoLC)30088363
    040
      
      
    a| ABC c| ABC d| OCLCG
    049
      
      
    a| UIUU
    050
      
    4
    a| TL521 b| .A3525 no. 7976
    100
    1
      
    a| Harvey, William D., d| 1934-
    245
    1
    0
    a| Experimental and numerical investigation of boundary-layer development and transition on the walls of a Mach 5 nozzle / c| William D. Harvey, Aubrey M. Cary, Jr., and Julius E. Harris.
    260
      
      
    a| Washington, D.C. : b| National Aeronautics and Space Administration ; a| [Springfield, Va. : b| For sale by the National Technical Information Service], c| 1975.
    300
      
      
    a| 86 p. : b| ill. ; c| 27 cm.
    490
    0
      
    a| NASA technical note ; v| NASA TN D-7976
    500
      
      
    a| Prepared at Langley Research Center.
    500
      
      
    a| Cover title.
    504
      
      
    a| Includes bibliographical references (p. 23-25).
    538
      
      
    a| Mode of access: Internet.
    650
      
    0
    a| Aerodynamics, Supersonic.
    650
      
    0
    a| Aerodynamics, Hypersonic.
    650
      
    0
    a| Jet nozzles.
    650
      
    0
    a| Transition flow.
    650
      
    0
    a| Boundary layer.
    700
    1
      
    a| Harris, Julius E.
    700
    1
      
    a| Cary, Aubrey M.
    710
    2
      
    a| Langley Research Center.
    974
      
      
    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106917096 y| 1975 r| pd q| bib

Access online

Google Preview