TY - GEN
T1 - The effects of insulation thickness on heat transfer for thermal protection system
AU - Liu, Shuang
AU - Zhang, Boming
AU - Xie, Weihua
PY - 2010
Y1 - 2010
N2 - The effects of insulation thickness are investigated with potential application in thermal protection system of hypersonic and re-entry vehicles. The traditional thermal protection system is modeled by the finite difference approach. Four different thicknesses of insulations' TPS are studied. The numerical calculation results show that structure temperature decreases as the insulation thickness increases as well as temperature difference increases, however, this effect weakens as the insulation thickness increased.
AB - The effects of insulation thickness are investigated with potential application in thermal protection system of hypersonic and re-entry vehicles. The traditional thermal protection system is modeled by the finite difference approach. Four different thicknesses of insulations' TPS are studied. The numerical calculation results show that structure temperature decreases as the insulation thickness increases as well as temperature difference increases, however, this effect weakens as the insulation thickness increased.
UR - https://www.scopus.com/pages/publications/79952141375
U2 - 10.1109/ISSCAA.2010.5633253
DO - 10.1109/ISSCAA.2010.5633253
M3 - 会议稿件
AN - SCOPUS:79952141375
SN - 9781424460441
T3 - ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
SP - 392
EP - 397
BT - ISSCAA2010 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics
T2 - 3rd International Symposium on Systems and Control in Aeronautics and Astronautics, ISSCAA2010
Y2 - 8 June 2010 through 10 June 2010
ER -