NACA-RM-E57k19

NACA-RM-E57k19
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  • 176 Downloads
  • 1.87 MB File Size
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  • December 4, 2015 Create Date
  • December 4, 2015 Last Updated
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National Advisory Committee for Aeronautics, Research Memorandum - Effects of Surface Roughness and Extreme Cooling on Boundary Layer Transition for 15deg Cone Cylinder in Free Flight at Mach Numbers to 7.6

naca-rm-e57k19 Effects of Surface Roughness and Extreme Cooling on Boundary-Layer Transition for 15° Cone-Cylinder in Free Flight at Mach Numbers to 7.6

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NACA-RM-E57k19

NACA-RM-E57k19
  • Version
  • 176 Downloads
  • 1.87 MB File Size
  • 1 File Count
  • December 4, 2015 Create Date
  • December 4, 2015 Last Updated
▼ Scroll for Details ▼

National Advisory Committee for Aeronautics, Research Memorandum - Effects of Surface Roughness and Extreme Cooling on Boundary Layer Transition for 15deg Cone Cylinder in Free Flight at Mach Numbers to 7.6

naca-rm-e57k19 Effects of Surface Roughness and Extreme Cooling on Boundary-Layer Transition for 15° Cone-Cylinder in Free Flight at Mach Numbers to 7.6

FileAction
naca-rm-e57k19.pdfDownload 
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