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FLIGHT PERFORMANCE OF THE REIMEI MICROSATELLITE ATTITUDE DETERMINATION SYSTEM
Establishment of FE bolt modeling method for crankcase strength analysis
2001-01-0143 Study on Lean Burn Gas Engine Using Pilot Oil as the Ignition Source
Effects of Particle Size on Microstructure of the Matrix Alloy in Aluminium Matrix Composites
Vehicle Interior Noise Prediction Using Sound Intensity Measurement
Electro Magnetic Formation Flight for LEO Satellites
Development of dual flow system of Diesel particulate filter made of porous metal