Item Details

Investigation of the Subsonic and Supersonic Release Characteristics of an Externally Carried Fuel Tank From a 1/40-Scale Model of a Bomber Airplane

by William F. Hinson
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration, 1961.
Language
English
Series
NASA Technical Memorandum
SuDoc Number
NAS 1.15:X-354
Description
129 p. : ill. ; 26 cm.
Mode of access: Internet.
Notes
  • "January 1961."
  • Cover title.
  • Includes bibliographical references (p. 11).
Series Statement
NASA technical memorandum ; X-354
Other Forms
Full text also available online. Address as of 11/11/2010: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660010438_1966010438.pdf.
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

  • LEADER 01650nam a2200421Ia 4500
    001 011449598
    003 MiAaHDL
    005 20141009010000.0
    006 m d
    007 cr bn ---auaua
    008 101111s1961 dcua bt f000 0 eng d
    035
      
      
    a| sdr-uiuc6405493
    035
      
      
    a| (OCoLC)680498803
    040
      
      
    a| UIU c| UIU
    049
      
      
    a| UIUU
    086
    0
      
    a| NAS 1.15:X-354
    100
    1
      
    a| Hinson, William F.
    245
    1
    0
    a| Investigation of the subsonic and supersonic release characteristics of an externally carried fuel tank from a 1/40-scale model of a bomber airplane / c| by William F. Hinson.
    260
      
      
    a| Washington, D.C. : b| National Aeronautics and Space Administration, c| 1961.
    300
      
      
    a| 129 p. : b| ill. ; c| 26 cm.
    490
    0
      
    a| NASA technical memorandum ; v| X-354
    500
      
      
    a| "January 1961."
    500
      
      
    a| Cover title.
    504
      
      
    a| Includes bibliographical references (p. 11).
    530
      
      
    a| Full text also available online. Address as of 11/11/2010: u| http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19660010438_1966010438.pdf.
    538
      
      
    a| Mode of access: Internet.
    650
      
    0
    a| Angle of attack (Aerodynamics)
    650
      
    0
    a| Bombers.
    650
      
    0
    a| Airplanes x| Fuel tanks x| Testing.
    650
      
    0
    a| Aerodynamics, Supersonic.
    710
    2
      
    a| Langley Research Center.
    974
      
      
    b| UIU c| UIUC d| 20161007 s| google u| uiug.30112104457848 y| 1961 r| pd q| bib

Access online

Google Preview