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Influence Of Oscillation Amplitude And Mach Number On The Unsteady Transition On A Pitching Rotor Blade Airfoil

Influence Of Oscillation Amplitude And Mach Number On The Unsteady Transition On A Pitching Rotor Blade Airfoil

  • Presented at Forum 69
  • 13 pages
  • SKU # : 69-2013-266

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Influence Of Oscillation Amplitude And Mach Number On The Unsteady Transition On A Pitching Rotor Blade Airfoil

Authors / Details: Kai Richter, Stefan Koch and Anthony Donald Gardner, German Aerospace Center (DLR)