naca-rm-a52k14

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National Advisory Committee for Aeronautics, Research Memorandum - Experimental Investigation of the Aerodynamic Characteristics of an Air to Air Missile Employing Cruciform Wings and Tail of Rectangular Plan Form at Mach Numbers of 1.4 and 1.9

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naca-rm-a52k14

  • Version
  • 45 Downloads
  • 977.93 KB File Size
  • 1 File Count
  • August 13, 2017 Create Date
  • August 13, 2017 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Research Memorandum - Experimental Investigation of the Aerodynamic Characteristics of an Air to Air Missile Employing Cruciform Wings and Tail of Rectangular Plan Form at Mach Numbers of 1.4 and 1.9

FileAction
naca-rm-a52k14 Experimental Investigation of the Aerodynamic Characteristics of an Air to Air Missile Employing Cruciform Wings and.pdfDownload 
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