naca-rm-l57a25

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National Advisory Committee for Aeronautics, Research Memorandum - Supersonic Aerodynamic Characteristics of a Low Drag Aircraft Configuration having an Arrow Wing of Aspect Ratio 1.86 and a Body of Fineness Ratio 20

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naca-rm-l57a25

  • Version
  • 58 Downloads
  • 1.71 MB File Size
  • 1 File Count
  • October 13, 2017 Create Date
  • October 13, 2017 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Research Memorandum - Supersonic Aerodynamic Characteristics of a Low Drag Aircraft Configuration having an Arrow Wing of Aspect Ratio 1.86 and a Body of Fineness Ratio 20

FileAction
naca-rm-l57a25 Supersonic Aerodynamic Characteristics of a Low Drag Aircraft Configuration having an Arrow Wing of Aspect Ratio 1.86 and a Body of Fineness Ratio 20.pdfDownload 
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