Item Details

Wind Tunnel Investigation of the Interaction and Breakdown Characteristics of Slender-Wing Vortices at Subsonic, Transonic, and Supersonic Speeds

Gary E. Erickson
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.
Language
English
Series
NASA Technical Paper
Description
222 p. : ill. ; 28 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • Includes bibliographical references (p. 20-21).
Series Statement
NASA technical paper ; 3114
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

  • LEADER 01681cam a2200433Ia 4500
    001 011423807
    003 MiAaHDL
    005 20141013010000.0
    006 m d
    007 cr bn ---auaua
    008 911230s1991 dcua b f000 0 eng d
    035
      
      
    a| sdr-uiuc6354101
    035
      
      
    a| (OCoLC)25028147
    040
      
      
    a| ABC c| ABC d| LVB d| TOL
    049
      
      
    a| UIUU
    090
      
      
    a| TL521.3 b| .N18 no. 3114
    100
    1
      
    a| Erickson, Gary E.
    245
    1
    0
    a| Wind tunnel investigation of the interaction and breakdown characteristics of slender-wing vortices at subsonic, transonic, and supersonic speeds / c| Gary E. Erickson.
    260
      
      
    a| Washington, D.C. : b| National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, c| 1991.
    300
      
      
    a| 222 p. : b| ill. ; c| 28 cm.
    490
      
    0
    a| NASA technical paper ; v| 3114
    500
      
      
    a| Prepared at Langley Research Center.
    504
      
      
    a| Includes bibliographical references (p. 20-21).
    538
      
      
    a| Mode of access: Internet.
    650
      
    6
    a| Avions x| Ailes delta x| Essais.
    650
      
    6
    a| Aérodynamique.
    650
      
    6
    a| Tourbillons (Mécanique des fluides)
    650
      
    0
    a| Airplanes x| Wings, Triangular x| Testing.
    650
      
    0
    a| Aerodynamics.
    650
      
    0
    a| Vortex-motion.
    710
    2
      
    a| Langley Research Center.
    974
      
      
    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106710814 y| 1991 r| pd q| bib

Access online

Google Preview