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H. O. Palme

  • An approximate method for the determination of the increase of maximum lift on thin profiles due to trailing edge flapsAn approximate method for the determination of the increase of maximum lift on thin profiles due to trailing edge flaps
  • Approximate methods to transform air inlet losses measured in low speed wind tunnels to varying flight conditionsApproximate methods to transform air inlet losses measured in low speed wind tunnels to varying flight conditions
  • Maximum lift for landing of swept wind aeroplanesMaximum lift for landing of swept wind aeroplanes
  • Summary of stalling characteristics and maximum lift of wings at low speedsSummary of stalling characteristics and maximum lift of wings at low speeds
  • Summary of wind tunnel data for high-lift devices on swept wingsSummary of wind tunnel data for high-lift devices on swept wings