| Citation: | LIN Jiaming, ZHANG Yi, YUE Ting, et al. Effect of asymmetric factors on carrier-based aircraft catapult launch safety[J]. Journal of Beijing University of Aeronautics and Astronautics, 2018, 44(2): 363-374. doi: 10.13700/j.bh.1001-5965.2017.0391(in Chinese)
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Asymmetric factors lead to lateral-directional departure after catapult launch, and affect longitudinal flyaway characteristics as well. Principle analysis and numerical simulation are conducted to reveal yawing movement characteristics during deck run and lateral-directional departure characteristics in catapult flyaway, with the consideration of three typical factors, such as off-center position, catapult runway angle and deck roll. According to the safety requirements of sink off bow and bank angle, safe wind over deck (WOD) envelope is figured through numerical simulation under different takeoff conditions. Simulation results indicate that lower boundary of the envelope is limited by maximum sink off bow, left and right boundary is restricted to maximum bank angle, and upper boundary is determined by constant wind at sea level. The range of safe WOD's direction and speed would be obviously narrowed due to off-center position or deck roll.
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