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System Integration of a Safe, High Power, Lithium Ion Main Battery into a Civil Aviation Aircraft

SAE International Journal of Aerospace

  • Journal Article
  • 2010-01-1770
Published 2010-11-02 by SAE International in United States
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Reduced Vertical Separation Minimum for General Aviation Aircraft

Published 1997-05-01 by SAE International in United States
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Environmental Durability of Aircraft Aluminum Alloy Skin Materials

Published 1993-05-01 by SAE International in United States
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Effect of an Isolated Shell on Interior Noise levels in a Turboprop Aircraft

Published 1989-04-01 by SAE International in United States
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Flight Test Investigations of a Wing Designed for Natural Laminar Flow

Published 1987-05-01 by SAE International in United States
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Further Results of Natural Laminar Flow Flight Test Experiments

Published 1985-04-01 by SAE International in United States
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Experimental Verification of Program KRASH-A Mathematical Model for General Aviation Structural Crash Dynamics

Published 1979-02-01 by SAE International in United States
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Weather Radar for Light Centerline Thrust Aircraft

Published 1977-02-01 by SAE International in United States
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The Influence of Design Parameters on Light Propeller Aircraft Noise

Published 1977-02-01 by SAE International in United States
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General Aviation Fatigue Loads-A Comparison of Analytical and Recorded Spectra

Published 1977-02-01 by SAE International in United States
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