TY - JOUR
AU - Guofeng, Wang
AB - The integrated thermal management system for a certain type of aircraft was studied. The integrated thermal management system, which takes fuel oil as the main heat sink, thermal protection structure and liquid evaporator as auxiliary heat sink, can comprehensively control and manage the heat of the whole aircraft. The mathematical model for simulation of integrated thermal management system was established. The simulation model of the system was built based on Flowmaster software for calculation. Results show that the system proposed in this paper can meet the overall thermal requirements of the aircraft, and provide a reference for the design of the aircraft integrated thermal management system and its subsystems.
TI - Modeling and simulation of aircraft integrated thermal management system
JF - Journal of Physics: Conference Series
DO - 10.1088/1742-6596/1314/1/012107
DA - 2019-10-01
UR - https://www.deepdyve.com/lp/iop-publishing/modeling-and-simulation-of-aircraft-integrated-thermal-management-II0cdnd6Zr
SP - 012107
VL - 1314
IS - 1
DP - DeepDyve
ER -