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Langley Aeronautical Laboratory.

  • Aerodynamic theory and its application to flutterAerodynamic theory and its application to flutter
  • Estimates Of The Vertical Tail-loads Of A Bell P-63A-1 Airplane (AAF No. 42-68889) In Accelerated Rolling Maneuvers Based On Flight Tests With Two Vertical-tail ArrangementsEstimates Of The Vertical Tail-loads Of A Bell P-63A-1 Airplane (AAF No. 42-68889) In Accelerated Rolling Maneuvers Based On Flight Tests With Two Vertical-tail Arrangements
  • Measurement Of Flying Qualities Of A De Havilland Mosquito F-8 Airplane (AAF No. 43-334960) IIMeasurement Of Flying Qualities Of A De Havilland Mosquito F-8 Airplane (AAF No. 43-334960) II
  • Measurement Of Flying Qualities Of A Dehavilland Mosquito F-8 Airplane (AAF No. 43-334960) IMeasurement Of Flying Qualities Of A Dehavilland Mosquito F-8 Airplane (AAF No. 43-334960) I
  • Measurement Of Flying Qualities Of A Douglas A-26B Airplane (AAF No. 41-39120) IMeasurement Of Flying Qualities Of A Douglas A-26B Airplane (AAF No. 41-39120) I
  • Measurement Of Flying Qualities Of A Douglas A-26B Airplane (AAF No. 41-39120) IIIMeasurement Of Flying Qualities Of A Douglas A-26B Airplane (AAF No. 41-39120) III
  • Measurement Of Flying Qualities Of A Douglas Douglas A-26B Airplane (AAF No. 41-39120) IIMeasurement Of Flying Qualities Of A Douglas Douglas A-26B Airplane (AAF No. 41-39120) II
  • Recent research on the determination of natural modes and frequencies of aircraft wing structuresRecent research on the determination of natural modes and frequencies of aircraft wing structures