Item Details

Performance of a 1.57-Pressure-Ratio Transonic Fan Stage With a Screen-Induced 90 ̊Circumferential Inlet Flow Distribution

Nelson L. Sanger
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], 1976.
Language
English
Series
NASA Technical Note
Description
iii, 73 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at Lewis Research Center.
  • Cover title.
  • Includes bibliographical references (p. 28).
Series Statement
NASA technical note ; NASA TN D-8163
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

  • LEADER 01632nam a2200421Ia 4500
    001 011443796
    003 MiAaHDL
    005 20141009010000.0
    006 m d
    007 cr bn ---auaua
    008 950210s1976 dcua b f000 0 eng d
    035
      
      
    a| sdr-uiuc6396516
    035
      
      
    a| (OCoLC)31967433
    040
      
      
    a| ABC c| ABC
    049
      
      
    a| UIUU
    050
      
    4
    a| TL521 b| .A3525 no. 8163
    100
    1
      
    a| Sanger, Nelson L.
    245
    1
    0
    a| Performance of a 1.57-pressure-ratio transonic fan stage with a screen-induced 90 ̊circumferential inlet flow distribution / c| Nelson L. Sanger.
    260
      
      
    a| Washington, D.C. : b| National Aeronautics and Space Administration ; a| [Springfield, Va. : b| For sale by the National Technical Information Service], c| 1976.
    300
      
      
    a| iii, 73 p. : b| ill. ; c| 27 cm.
    490
    0
      
    a| NASA technical note ; v| NASA TN D-8163
    500
      
      
    a| Prepared at Lewis Research Center.
    500
      
      
    a| Cover title.
    504
      
      
    a| Includes bibliographical references (p. 28).
    538
      
      
    a| Mode of access: Internet.
    650
      
    0
    a| Aerodynamics, Transonic.
    650
      
    0
    a| Airplanes x| Turbojet engines x| Compressors.
    650
      
    0
    a| Compressors x| Aerodynamics.
    650
      
    0
    a| Compressors x| Performance.
    710
    2
      
    a| Lewis Research Center.
    974
      
      
    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106915611 y| 1976 r| pd q| bib

Access online

Google Preview