TY - GEN
T1 - Development of landing and taxiing response analysis system for aircraft with multi-wheels and multi-landing gears
AU - Wang, Hui
AU - Wang, Le
PY - 2013
Y1 - 2013
N2 - Based on the modularized conception, the landing and taxiing response analysis system for aircraft with multi-wheels and multi-landing gears was developed. Firstly, the submodels, such as the oil pole model, the buffer model, the tire model and the landing gear model should be built one by one; then, the fuselage model can be assembled by the submodels; finally, the landing and taxiing responses of the aircraft can be calculated under the specified initial conditions. An aircraft model with multi-wheels and multi-landing gears was adopted as an example to verify the feasibility and effectiveness of the software.
AB - Based on the modularized conception, the landing and taxiing response analysis system for aircraft with multi-wheels and multi-landing gears was developed. Firstly, the submodels, such as the oil pole model, the buffer model, the tire model and the landing gear model should be built one by one; then, the fuselage model can be assembled by the submodels; finally, the landing and taxiing responses of the aircraft can be calculated under the specified initial conditions. An aircraft model with multi-wheels and multi-landing gears was adopted as an example to verify the feasibility and effectiveness of the software.
KW - Aircraft with multi-wheels and multi-landing gears
KW - Dynamic analysis
KW - Landing and taxiing response
KW - Landing gear
KW - Software design
UR - https://www.scopus.com/pages/publications/84887512309
U2 - 10.4028/www.scientific.net/AMM.459.511
DO - 10.4028/www.scientific.net/AMM.459.511
M3 - 会议稿件
AN - SCOPUS:84887512309
SN - 9783037859230
T3 - Applied Mechanics and Materials
SP - 511
EP - 516
BT - Applied Mechanics and Mechanical Engineering IV
T2 - 2013 4th International Conference on Applied Mechanics and Mechanical Engineering, ICAMME 2013
Y2 - 11 October 2013 through 12 October 2013
ER -