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在“Elsevier电子期刊”中，命中：400条，耗时：0.0389868 秒

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1.A laminar kinetic energy transition model appropriate for hypersonic flow heat transfer

作者：Y.P. Qin^a ; C. Yan^a ; ^{yanchao@buaa.edu.cn} ; Z.H. Hao^a ; L. Zhou^b

关键词：Heat transfer ; Boundary layer transition ; Laminar kinetic energy ; Hypersonic

刊名：International Journal of Heat and Mass Transfer

出版年：2017

2.Numerical study of active flow control over a hypersonic backward-facing step using supersonic jet in near space

作者：Guang-ming Guo ^{guoming20071028@163.com} ; Hong Liu ; ^{hongliu@sjtu.edu.cn} ; Bin Zhang

关键词：Backward-facing step ; Flow characteristics ; Active flow control ; DSMC ; Near space

刊名：Acta Astronautica

出版年：2017

3.A study of performance parameters on drag and heat flux reduction efficiency of combinational novel cavity and opposing jet concept in hypersonic flows

作者：Xi-wan Sun ; Zhen-yun Guo ; Wei Huang ; ^{gladrain2001@163.com} ; Shi-bin Li ; Li Yan

关键词：Hypersonic flow ; Drag and heat reduction ; Forward-facing cavity ; Opposing jet ; Jet operating conditions ; Freestream angle of attack ; Physical dimensions

刊名：Acta Astronautica

出版年：2017

4.Experimental investigation of surface flow pattern on truncated cones in Mach 5 flow: Influence of truncation ratio

作者：Takahiro Ukai^a ; ^{Takahiro.Ukai@glasgow.ac.uk" class="auth_mail" title="E-mail the corresponding author} ; Hossein Zare-Behtash^a ; Konstantinos Kontis^a ; Leichao Yang^b ; Erinc Erdem^c

关键词：Truncated cone ; Pressure-sensitive paint ; Hypersonic flow

刊名：Experimental Thermal and Fluid Science

出版年：2017

5.Recent research progress on unstart mechanism, detection and control of hypersonic inlet

作者：Juntao Chang ; ¹ ; ^{changjuntao@hit.edu.cn} ; Nan Li² ; Kejing Xu² ; Wen Bao² ; Daren Yu²

关键词：Unstart flow mechanisms ; Hysteresis characteristics ; Margin characterization ; Unstart detection and control ; Flow control

刊名：Progress in Aerospace Sciences

出版年：2017

6.Collision partner selection schemes in DSMC: From micro/nano flows to hypersonic flows

作者：Ehsan Roohi ; ^{e.roohi@ferdowsi.um.ac.ir" class="auth_mail" title="E-mail the corresponding author} ; Stefan Stefanov

关键词：Rarefied flow ; Boltzmann equation ; Kac master equations ; DSMC ; Collision models ; Simplified Bernoulli trials ; Micro/nano flows ; Hypersonic flow

刊名：Physics Reports

出版年：2016

7.Experimental and numerical investigation of smooth turbine-based combined-cycle inlet mode transition

作者：Jun Liu ; Huacheng Yuan ; ^{yuan_hch7@sina.com} ; Zhengxu Hua ; Wenfang Chen ; Ning Ge

关键词：Air-breathing hypersonic propulsion system ; Turbine-based combined-cycle ; Inlet mode transition ; Wind tunnel test

刊名：Aerospace Science and Technology

出版年：2017

8.Analysis of dimensionality effect on shock wave boundary layer interaction in laminar hypersonic flows

作者：Bibin John^a ; Srikanth Surendranath^b ; Ganesh Natarajan^b ; Vinayak Kulkarni^b ; ^{vinayak@iitg.ernet.in}

关键词：Shock wave boundary layer interactions ; Laminar flow ; Hypersonics ; Bluntness ; Flow separation

刊名：International Journal of Heat and Fluid Flow

出版年：2016

9.A quasi-one-dimensional model for hypersonic reactive flow along the stagnation streamline

作者：Song Chen^a ; ^{chensong212@hotmail.com}Author Vitae ; Quanhua Sun^a ; ^b ; ^{qsun@imech.ac.cn}Author Vitae

关键词：Quasi-one-dimensional model ; Hypersonic ; Non-equilibrium ; Stagnation flow ; Shock stand-off distance

刊名：Chinese Journal of Aeronautics

出版年：2016

10.Hypersonic starting flow at high angle of attack

作者：Chenyuan Bai ^{bcy12@mails.tsinghua.edu.cn" class="auth_mail" title="E-mail the corresponding author}Author Vitae ; Ziniu Wu ; ^{ziniuwu@tsinghua.edu.cn" class="auth_mail" title="E-mail the corresponding author}Author Vitae

关键词：Hypersonic ; Normal force ; Shock waves ; Starting flow ; Unsteady flow

刊名：Chinese Journal of Aeronautics

出版年：2016

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