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A Flexible Fixture for Aircraft Wing Assembly Based on a Parallel Kinematic Machine (Exechon)

SAE International Journal of Aerospace

  • Journal Article
  • 2011-01-2555
Published 2011-10-18 by SAE International in United States
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Root Mean Square Response of Transducer Systems to Spectral Density Inputs

Published 1987-10-01 by SAE International in United States
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AFTI/F-16 Voice Interactive Avionics Evaluation

Published 1987-10-01 by SAE International in United States
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Advances in Flight Test Instrumentation and Analysis

Published 1987-10-01 by SAE International in United States
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Blast Induced Shock Testing on Mobile Communications Shelters

Published 1987-10-01 by SAE International in United States
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Development of Wing and Tail Configurations for Low Altitude Unmanned Research Aircraft (LAURA)

Published 1987-10-01 by SAE International in United States
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A Close-Coupled Canard, Technology Demonstration Aircraft for General Aviation Applications

Published 1987-10-01 by SAE International in United States
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Shock Tube Tests of a Kevlar Sandwich Panel and Comparison with Theory

Published 1987-10-01 by SAE International in United States
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Tactics and Equipment Evaluation

Published 1987-10-01 by SAE International in United States
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Lessons Learned from an Operational, Engine Monitoring System and Their, Correlation with Future Developments

Published 1987-10-01 by SAE International in United States
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