NACA-TN-4185

NACA-TN-4185
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  • 163 Downloads
  • 2.56 MB File Size
  • 1 File Count
  • December 4, 2015 Create Date
  • December 4, 2015 Last Updated
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National Advisory Committee for Aeronautics, Technical Notes - Wind-Tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack up to 13deg and at High Subsonic Mach Numbers, Including a stimating the Rolling Derivatives

naca-tn-4185 Wind-Tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack up to 13° and at High Subsonic Mach Numbers, Including a Semiempirical Method

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NACA-TN-4185

NACA-TN-4185
  • Version
  • 163 Downloads
  • 2.56 MB File Size
  • 1 File Count
  • December 4, 2015 Create Date
  • December 4, 2015 Last Updated
▼ Scroll for Details ▼

National Advisory Committee for Aeronautics, Technical Notes - Wind-Tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack up to 13deg and at High Subsonic Mach Numbers, Including a stimating the Rolling Derivatives

naca-tn-4185 Wind-Tunnel Investigation of Effect of Sweep on Rolling Derivatives at Angles of Attack up to 13° and at High Subsonic Mach Numbers, Including a Semiempirical Method

FileAction
naca-tn-4185.pdfDownload 
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