Zobrazeno 1 - 8
of 8
pro vyhledávání: '"Xiangren, Geng"'
Publikováno v:
Advances in Aerodynamics, Vol 3, Iss 1, Pp 1-10 (2021)
Abstract A scaled model of the X38-like configuration was simulated under hypersonic conditions for the direct simulation Monte Carlo method and the unified gas kinetic scheme. The inflow conditions considered several flow regimes, from the near-cont
Externí odkaz:
https://doaj.org/article/746672b48a944f7e96225dfe211dd2f1
Publikováno v:
Journal of Thermophysics and Heat Transfer. 32:156-160
This paper concerns the development of a novel hybrid hard sphere molecular model in direct simulation Monte Carlo technique. Usually, the variable hard sphere model is applied to simulate molecula...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::18521946c14cb9471ace1368be89475b
https://doi.org/10.2514/1.t5162
https://doi.org/10.2514/1.t5162
Study on the Temperature Field of Hypersonic Vehicle Structure with Aerothermoelasticity Deformation
Publikováno v:
DEStech Transactions on Materials Science and Engineering.
The malfunction of thermal protection system (TPS) caused by aerodynamic heating is a latent trouble to aircraft structure safety. Accurately predicting the structure temperature field is quite important for the TPS design of hypersonic vehicle. Sinc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5bf1c8ef12c48f68b5721031145571cd
https://doi.org/10.12783/dtmse/icmea2015/7363
https://doi.org/10.12783/dtmse/icmea2015/7363
Publikováno v:
21st AIAA International Space Planes and Hypersonics Technologies Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f68a1a2f9c8b338837156c3a2b10dfda
https://doi.org/10.2514/6.2017-2365
https://doi.org/10.2514/6.2017-2365
The malfunction of thermal protection system (TPS) caused by aerodynamic heating is a latent trouble to aircraft structure safety. Accurately predicting the structure temperature field is quite important for the TPS design of hypersonic vehicle. Sinc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::708d4de2e3cb51e36a0d07841c6d8417
Publikováno v:
Journal of Thermal Science and Technology. 7:262-271
The performance parameters of thermal protection system are essential for the design and optimization of high-speed aircraft. The flight-ground conversion is a valid method to provide the effective support to the design of the thermal protection stru
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::7562df153b6edaa3ee73f9327a8fd33d
https://doi.org/10.1299/jtst.7.262
https://doi.org/10.1299/jtst.7.262
Publikováno v:
Heat Transfer—Asian Research. 37:218-223
The establishment of a reasonable physical model and an effective solution scheme for the thermal corridor is very important to thermal protection structure design, trajectory selection, aerodynamic configuration optimization design, etc. The concept
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bf779e5297391ae2cab78f34cdd75051
https://doi.org/10.1002/htj.20203
https://doi.org/10.1002/htj.20203
Publikováno v:
AIP Conference Proceedings; 2014, Vol. 1628, p288-295, 8p, 3 Diagrams, 1 Chart, 9 Graphs