Zobrazeno 1 - 10
of 24
pro vyhledávání: '"Bangcheng, AI"'
Publikováno v:
Aerospace, Vol 10, Iss 7, p 654 (2023)
This paper presents a deep neural network-based online trajectory generation method for the aerodynamic characteristic description and terminal-area energy management of wave-rider aircrafts. First, the flight dynamics equations in the energy domain
Externí odkaz:
https://doaj.org/article/85e5ed63786b458390121678b0ec8ec7
Publikováno v:
Materials, Vol 14, Iss 11, p 3016 (2021)
In this study, pentamode metamaterials were proposed for thermal stress accommodation of alkali metal heat pipes. Sodium/Inconel 718 heat pipes with and without pentamode metamaterial reinforcement were designed and fabricated. Then, these heat pipes
Externí odkaz:
https://doaj.org/article/6a1c946181f94df5a01d2eb344b70cbb
Publikováno v:
In Journal of Sound and Vibration 13 October 2016 380:165-179
Publikováno v:
SCIENTIA SINICA Technologica. 52:292-302
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::13f94fc34f4aa52dc890e1e81fadb38d
https://doi.org/10.1360/sst-2021-0476
https://doi.org/10.1360/sst-2021-0476
Publikováno v:
Microgravity Science and Technology. 31:417-424
In this study, sodium/GH4099 heat pipes are proposed for nose cap cooling. X-51 nose cap-like sodium/GH4099 heat pipe spreaders were designed and prepared in China Academy of Aerospace Aerodynamics (CAAA). And their startup properties were tested at
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::87ee2d0be64d2de07f43f7a3f38aa5dd
https://doi.org/10.1007/s12217-019-09714-w
https://doi.org/10.1007/s12217-019-09714-w
Publikováno v:
Microgravity Science and Technology. 31:783-791
Cooling channel involved heat pipes, which synergistically combined the high conductivity of heat pipe and thermal efficiency of regenerative cooling, were considered for combustor cooling. In this study, cooling channels were fabricated in sodium/In
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::f06f360f534da39e4815ff65a21b6c1d
https://doi.org/10.1007/s12217-019-09709-7
https://doi.org/10.1007/s12217-019-09709-7
Publikováno v:
Chinese Journal of Aeronautics, Vol 32, Iss 4, Pp 815-825 (2019)
This paper attempts to develop a scaling procedure to measure structural vibration caused simultaneously by wall pressure fluctuations and the thermal load of hypersonic flow by a wind tunnel test. However, simulating the effect of thermal load is di
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::772ec0ca2b4c68780c7375ce946d1d06
http://www.sciencedirect.com/science/article/pii/S1000936119300573
http://www.sciencedirect.com/science/article/pii/S1000936119300573
Publikováno v:
International Journal of Heat and Mass Transfer. 129:480-490
Owing to the huge phase-change latent heat, transpiration cooling using liquid coolant has been widely recognized as an effective thermal protection approach for hypersonic vehicles. This paper presents a modified local thermal non-equilibrium two-ph
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::537613fd4b3dec8d5b2e44f40a9851aa
https://doi.org/10.1016/j.ijheatmasstransfer.2018.09.123
https://doi.org/10.1016/j.ijheatmasstransfer.2018.09.123
Publikováno v:
International Journal of Heat and Mass Transfer. 127:882-891
With the development of active thermal protection techniques (TPTs), optimization transpiration cooling (OTC) design, to enhance the cooling effect in stagnation regions and decrease coolant load, has become a critical issue in the research and devel
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::868053aa388fa174b3e991354dfd322a
https://doi.org/10.1016/j.ijheatmasstransfer.2018.07.134
https://doi.org/10.1016/j.ijheatmasstransfer.2018.07.134
Publikováno v:
Chinese Journal of Aeronautics, Vol 31, Iss 3, Pp 481-489 (2018)
This paper presents a new method for measuring the cabin noise of a structure in a wind tunnel. A method for scaling the cabin sound was derived to obtain the cabin noise of a structure, and the derivation of the scaling procedure was based on a theo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::b139a4aca0d0c22fb5b50a5b9d1fcd09
https://doi.org/10.1016/j.cja.2017.12.015
https://doi.org/10.1016/j.cja.2017.12.015