Study on the Impact of Missile Flight Mach to its Engine Thrust
Study on Effect of Shipborne Missile Launch Position Based on Fast Fourier Transform
Research on Initial Disturbance Influenced by Adapter Combined with Guide Rail
Optimization Maneuver Strategy which Make the Loss of Height of UAV Minimum after Engine Stopped
Modal Analysis on the Simulation of the Missile Launchers Based on ABAQUS
Dynamic Simulation Analysis of Shipborne Missile Launching under High-Wave-Level Environment
Design of the Tracked Vehicle Based on the STM32
Analysis and Calculation of Tracked Vehicle Steering-Load Based on Conditions of Tracks' Slip