Item Details

Flight Reynolds Number Effects on a Contoured Boattail Nozzle at Subsonic Speeds

by Roger Chamberlin
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], 1974.
Language
English
Series
NASA Technical Memorandum
SuDoc Number
NAS 1.15:X-3053
Description
23 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at Lewis Research Center.
  • Cover title.
  • Includes bibliographical references (p. 8-9).
Series Statement
NASA technical memorandum ; NASA TM X-3053
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

  • LEADER 01713cam a2200469Ia 4500
    001 011424391
    003 MiAaHDL
    005 20141013010000.0
    006 m d
    007 cr bn ---auaua
    008 930513s1974 dcua b f000 0 eng d
    029
    1
      
    a| GBVCP b| 607849746
    035
      
      
    a| sdr-uiuc6359388
    035
      
      
    a| (OCoLC)28101848
    040
      
      
    a| ABC c| ABC d| LHL
    049
      
      
    a| UIUU
    050
      
    4
    a| TL521.3.T4 b| A3 no. 3053
    086
    0
      
    a| NAS 1.15:X-3053
    100
    1
      
    a| Chamberlin, Roger.
    245
    1
    0
    a| Flight Reynolds number effects on a contoured boattail nozzle at subsonic speeds / c| by Roger Chamberlin.
    260
      
      
    a| Washington, D.C. : b| National Aeronautics and Space Administration ; a| [Springfield, Va. : b| For sale by the National Technical Information Service], c| 1974.
    300
      
      
    a| 23 p. : b| ill. ; c| 27 cm.
    490
    0
      
    a| NASA technical memorandum ; v| NASA TM X-3053
    500
      
      
    a| Prepared at Lewis Research Center.
    500
      
      
    a| Cover title.
    504
      
      
    a| Includes bibliographical references (p. 8-9).
    538
      
      
    a| Mode of access: Internet.
    650
      
    0
    a| Delta Dart (Jet fighter plane)
    650
      
    0
    a| Airplanes x| Nacelles.
    650
      
    0
    a| Reynolds number.
    650
      
    0
    a| Aerodynamics, Transonic.
    650
      
    0
    a| Drag (Aerodynamics)
    650
      
    0
    a| Airplanes x| Turbojet engines.
    650
      
    0
    a| Jet nozzles.
    710
    2
      
    a| Lewis Research Center.
    974
      
      
    b| UIU c| UIUC d| 20161008 s| google u| uiug.30112106659904 y| 1974 r| pd q| bib

Access online

Google Preview