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Suresh, K.
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An Efficient Analysis Method for Prediction and Structural Dimensioning of Wing-Pylon-Adapter-Rocket Pod Assembly Subjected to Shock Loading

Published 2016-09-20 by SAE International in United States
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Preliminary Design and Vibration Study of Micro-Satellite Structure

Published 2005-10-03 by SAE International in United States
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Test Approach for the Mechanical Qualification of a Micro-Satellite Structure and Subsystems

Published 2006-08-30 by SAE International in United States
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Conceptual Design, Material, and Structural Optimization of a Naval Fighter Nose Landing Gear for the Estimated Static Loads

SAE International Journal of Aerospace

  • Journal Article
  • 01-12-02-0009
Published 2019-12-13 by SAE International in United States
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ERRATA

SAE International Journal of Aerospace

  • Journal Article
  • 01-12-02-0009.1
Published 2020-05-12 by SAE International in United States
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