Item Details

An Experimental Investigation at a Mach Number of 4.95 of Flow in the Vicinity of a 90 Degree Interior Corner Alined With the Free-Stream Velocity

by P. Calvin Stainback
Format
Book; Government Document; Online; EBook
Published
Washington, [D.C.] : National Aeronautics and Space Administration, 1960.
Language
English
Series
NASA Technical Note
Description
30 p. : ill. ; 26 cm.
Mode of access: Internet.
Notes
  • "NASA TN D-184."
  • "Langley Research Center, Langley Field, Va."
  • "February 1960."
  • Title from cover.
  • Includes bibliographical references (p. 16-17).
Series Statement
NASA technical note ; D-184
Other Forms
Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 12/20/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068207_1989068207.pdf.
Logo for Copyright Not EvaluatedCopyright Not Evaluated
Technical Details

  • LEADER 02160nam a2200553Ia 4500
    001 011433194
    003 MiAaHDL
    005 20141009010000.0
    006 m d
    007 cr bn ---auaua
    008 061221s1960 dcua bt f000 0 eng d
    024
    8
      
    a| 89N70580
    024
    8
      
    a| 19890068207
    035
      
      
    a| sdr-uiuc6390380
    035
      
      
    a| (OCoLC)77221825
    040
      
      
    a| FER c| FER
    049
      
      
    a| UIUU
    100
    1
      
    a| Stainback, P. Calvin.
    245
    1
    3
    a| An experimental investigation at a Mach number of 4.95 of flow in the vicinity of a 90 degree interior corner alined with the free-stream velocity / c| by P. Calvin Stainback.
    260
      
      
    a| Washington, [D.C.] : b| National Aeronautics and Space Administration, c| 1960.
    300
      
      
    a| 30 p. : b| ill. ; c| 26 cm.
    490
      
    0
    a| NASA technical note ; v| D-184
    500
      
      
    a| "NASA TN D-184."
    500
      
      
    a| "Langley Research Center, Langley Field, Va."
    500
      
      
    a| "February 1960."
    500
      
      
    a| Title from cover.
    504
      
      
    a| Includes bibliographical references (p. 16-17).
    530
      
      
    a| Also available online from the NASA Technical Reports Server (http://ntrs.nasa.gov/). Address as of 12/20/06: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890068207_1989068207.pdf.
    538
      
      
    a| Mode of access: Internet.
    650
      
    7
    a| Static pressure. 2| nasat
    650
      
    7
    a| Stagnation temperature. 2| nasat
    650
      
    7
    a| Reynolds number. 2| nasat
    650
      
    7
    a| Mach number. 2| nasat
    650
      
    7
    a| Aerodynamic interference. 2| nasat
    650
      
    7
    a| Laminar flow. 2| nasat
    650
      
    7
    a| Shock layers. 2| nasat
    650
      
    7
    a| Hypersonic heat transfer. 2| nasat
    650
      
    7
    a| Free flow. 2| nasat
    650
      
    7
    a| Corner flow. 2| nasat
    650
      
    7
    a| Boundary layer flow. 2| nasat
    710
    2
      
    a| Langley Research Center.
    974
      
      
    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106773556 z| v.184 y| 1960 r| pd q| bib

Access online

Google Preview