Item Details

Sound Radiation From a High-Speed Axial-Flow Fan Due to the Inlet Turbulence Quadrupole Interaction

by Marvin E. Goldstein, Burt M. Rosenbaum, and Lynn U. Albers
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]
Language
English
Series
NASA Technical Note
Description
46 p. : ill. ; 27 cm.
Mode of access: Internet.
Notes
  • Prepared at Lewis Research Center.
  • Cover title.
  • Includes bibliographical references (p. 39).
Series Statement
NASA technical note ; NASA TN D-7667
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

  • LEADER 01769nam a2200445Ia 4500
    001 011446962
    003 MiAaHDL
    005 20141009010000.0
    006 m d
    007 cr bn ---auaua
    008 920421s1974 dcua b f000 0 eng d
    035
      
      
    a| sdr-uiuc6406425
    035
      
      
    a| (OCoLC)25685017
    040
      
      
    a| ABC c| ABC
    049
      
      
    a| UIUU
    050
      
    4
    a| TL521 b| .A3525 no. 7667
    100
    1
      
    a| Goldstein, Marvin E.
    245
    1
    0
    a| Sound radiation from a high-speed axial-flow fan due to the inlet turbulence quadrupole interaction / c| by Marvin E. Goldstein, Burt M. Rosenbaum, and Lynn U. Albers.
    260
      
      
    a| Washington, D.C. : b| National Aeronautics and Space Administration ; a| [Springfield, Va. : b| For sale by the National Technical Information Service],
    300
      
      
    a| 46 p. : b| ill. ; c| 27 cm.
    490
    0
      
    a| NASA technical note ; v| NASA TN D-7667
    500
      
      
    a| Prepared at Lewis Research Center.
    500
      
      
    a| Cover title.
    504
      
      
    a| Includes bibliographical references (p. 39).
    538
      
      
    a| Mode of access: Internet.
    650
      
    0
    a| Airplanes x| Turbojet engines.
    650
      
    0
    a| Compressors x| Aerodynamics x| Mathematical models.
    650
      
    0
    a| Compressors x| Blades x| Noise x| Mathematical models.
    650
      
    0
    a| Axial flow compressors x| Noise x| Mathematical models.
    700
    1
      
    a| Albers, Lynn U.
    700
    1
      
    a| Rosenbaum, Burt M.
    710
    2
      
    a| Lewis Research Center.
    974
      
      
    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106886044 y| 1974 r| pd q| bib

Access online

Google Preview