Item Details

Effect of Leading-Edge Load Constraints on the Design and Performance of Supersonic Wings

Christine M. Carden
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985.
Language
English
Series
NASA Technical Paper
SuDoc Number
NAS 1.60:2446
Description
iii, 74 p. : ill. ; 28 cm.
Mode of access: Internet.
Notes
  • Prepared at Langley Research Center.
  • "July 1985"--Cover.
  • Includes bibliographical references (p. 7).
Series Statement
NASA technical paper ; 2446
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

  • LEADER 01768cam a2200445Ia 4500
    001 011425581
    003 MiAaHDL
    005 20141013010000.0
    006 m d
    007 cr bn ---auaua
    008 951115s1985 dcua b f000 0 eng d
    035
      
      
    a| sdr-uiuc6361983
    035
      
      
    a| (OCoLC)33481740
    040
      
      
    a| ABC c| ABC d| OCL
    049
      
      
    a| UIUU
    086
    0
      
    a| NAS 1.60:2446
    090
      
      
    a| TL521.3 b| .N18 no. 2446
    100
    1
      
    a| Darden, Christine M.
    245
    1
    0
    a| Effect of leading-edge load constraints on the design and performance of supersonic wings / c| Christine M. Carden.
    260
      
      
    a| Washington, D.C. : b| National Aeronautics and Space Administration, Scientific and Technical Information Branch ; a| Springfield, Va. : b| For sale by the National Technical Information Service, c| 1985.
    300
      
      
    a| iii, 74 p. : b| ill. ; c| 28 cm.
    490
      
    0
    a| NASA technical paper ; v| 2446
    500
      
      
    a| Prepared at Langley Research Center.
    500
      
      
    a| "July 1985"--Cover.
    504
      
      
    a| Includes bibliographical references (p. 7).
    538
      
      
    a| Mode of access: Internet.
    650
      
    0
    a| Airplanes x| Wings x| Design and construction.
    650
      
    0
    a| Aerodynamics, Supersonic.
    650
      
    0
    a| Aerodynamic load.
    650
      
    0
    a| Leading edges (Aerodynamics)
    650
      
    0
    a| Airplanes x| Wings x| Testing v| Statistics.
    710
    2
      
    a| Langley Research Center.
    974
      
      
    b| UIU c| UIUC d| 20200404 s| google u| uiug.30112105146838 y| 1985 r| pd q| bib t| US fed doc--NTIS: pubdate < 2014