Design and Analysis of Aircraft Active Landing Gear to Study the Dynamic Response of the Aircraft During Heavy Landing, Taxing on Uneven / Random Runway Surfaces
Completed
Role: Co-Principal Investigator
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HYBRID ROCKET WITH PROPELLANTS AS PREMIXED LIQUEFYING FUEL AND OXIDIZER
T. SELVAKUMARAN
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Patent No. :
508686
Filed :
08-10-2018
Published :
19-10-2018Granted
Scholarly Publications
Self Supervised Learning for Structural Integrity Assessment of UAVs in Extended Missions