共 32 条
- [1] ZHAO J, SUN X C, ZHANG J, Et al., Research advances on heat and mass transfer coupling effect at gas-solid interface for thermal protection materials, Acta Aeronautica et Astronautica Sinica, 43, 10, (2022)
- [2] YE Y D., Advances and prospects in hypersonic aerodynamics, Chinese Science Bulletin, 60, 12, pp. 1095-1103, (2015)
- [3] LI H Y, TANG Z G, YANG Y G, Et al., Problems of numerical simulation of high-temperature gas flow fields for hypersonic vehicles, Acta Aeronautica et Astronautica Sinica, 36, 1, pp. 176-191, (2015)
- [4] DONG W Z, GAO T S, DING M S, Et al., Numerical study of coupled surface temperature distribution and aerodynamic heat for hypersonic vehicles, Acta Aeronautica et Astronautica Sinica, 36, 1, pp. 311-324, (2015)
- [5] LAUB B, VENKATAPATHY E., Thermal protection system technology and facility needs for demanding future planetary missions, International Workshop on Planetary Probe Atmospheric Entry and Descent Trajectory Analysis and Science, pp. 239-247, (2004)
- [6] WANG Y, YANG Y H, FENG Z H., Current status and further trend of thermal protection materials for deep space exploration, Aerospace Materials & Technology, 43, 5, pp. 1-10, (2013)
- [7] JOHNSON S M., Thermal protection materials:Development, characterization and evaluation: ARC-E-DAATN5732, (2012)
- [8] REYNIER P., Convective blockage during Earth reentry:A review, 40th AIAA Thermophysics Conference, (2008)
- [9] REYNIER P., Survey of convective blockage for planetary entries, Acta Astronautica, 83, pp. 175-195, (2013)
- [10] BREWER R A, BRANT D N., Thermal protection system for the Galileo mission atmospheric entry probe: AIAA-1980-0358, (1980)