Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Kuangshi Chen"'
Publikováno v:
Chinese Journal of Aeronautics. 36:42-62
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::09591fbb330daee98dcd4419b8837ea3
https://doi.org/10.1016/j.cja.2022.11.015
https://doi.org/10.1016/j.cja.2022.11.015
Publikováno v:
Acta Astronautica. 202:58-76
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::99326d09cc6fb3b49a3d8314dde3fe7e
https://doi.org/10.1016/j.actaastro.2022.09.060
https://doi.org/10.1016/j.actaastro.2022.09.060
Publikováno v:
AIAA Journal. 59:2014-2026
This Paper is a computational investigation of a scramjet nozzle design based on maximum thrust theory and its feasibility analysis. A new design method for a two-dimensional complete thrust-optimi...
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::61599a169eb353e2abef46c1f1c2677b
https://doi.org/10.2514/1.j059846
https://doi.org/10.2514/1.j059846
Publikováno v:
Physics of Fluids. 35:016118
Supersonic axisymmetric expansion flow is a typical and fundamental issue in gas dynamics. It plays a vital role in the high-speed external and internal flow fields regarding the contour design and performance evaluation of supersonic/hypersonic vehi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0c3a4839761ec7e6ef72eab4609b1345
https://doi.org/10.1063/5.0134698
https://doi.org/10.1063/5.0134698
Publikováno v:
Aerospace Science and Technology. 127:107690
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c3a86276beaafbcc3b7837c991827302
https://doi.org/10.1016/j.ast.2022.107690
https://doi.org/10.1016/j.ast.2022.107690
Publikováno v:
Physics of Fluids. 34:076114
A high-temperature effect is crucial in cold-to-hot correlation for thrust nozzles to employ experimental data of cold flow to predict the real flight performance of hot gas. The high-temperature nozzle flow behaves beyond the classical gas dynamics
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::689f3b881e68f1f4c4b6bd861da4e363
https://doi.org/10.1063/5.0098894
https://doi.org/10.1063/5.0098894
Publikováno v:
Journal of Fluids and Structures. 95:102983
This study develops a two-way loosely coupled aeroelastic analysis framework based on a finite-volume fluid solver, a nonlinear finite-element solid solver and the Mesh-based parallel Code Coupling Interface. Research focuses on aeroelastic behaviour
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::caf6f758cbd2ce29ae7682c87c8ea742
https://doi.org/10.1016/j.jfluidstructs.2020.102983
https://doi.org/10.1016/j.jfluidstructs.2020.102983