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在“Elsevier电子期刊”中，命中：404条，耗时：0.095956 秒

在所有数据库中总计命中：4,965条

1.Heat transfer and pressure loss in swirl tubes with one and multiple tangential jets pertinent to gas turbine internal cooling

作者：Yu Rao^a ; ^{yurao@sjtu.edu.cn} ; Christoph Biegger^b ; Bernhard Weigand^b

关键词：Gas turbine cooling ; Swirl tube ; Heat transfer ; Pressure loss ; Tangential jet

刊名：International Journal of Heat and Mass Transfer

出版年：2017

2.Effect of purge flow on endwall flow and heat transfer characteristics of a gas turbine blade

作者：Liming Song ; Peiyuan Zhu ; Jun Li ; ^{junli@mail.xjtu.edu.cn" class="auth_mail" title="E-mail the corresponding author} ; Zhenping Feng

关键词：Purge flow ; Film cooling ; Endwall heat transfer ; Gas turbine blade ; Secondary vortexes ; Numerical simulation

刊名：Applied Thermal Engineering

出版年：2017

3.Numerical investigation of the effects of discrete guide vanes on the control of heat transfer on the tip surface of a turbine blade

作者：Seok Min Choi ; Eui Yeop Jung ; Heeyoon Chung ; Hyung Hee Cho ; ^{hhcho@yonsei.ac.kr}

关键词：Gas turbine ; Heat transfer ; Guide vane ; Tip surface ; Cooling

刊名：International Journal of Thermal Sciences

出版年：2017

4.Numerical prediction on mist/steam cooling in a square ribbed channel at real gas turbine operational conditions

作者：Tieyu Gao^a ; ^{sunmoon@mail.xjtu.edu.cn} ; Junxiong Zeng^a ; Jun Li^a ; Jianying Gong^b

关键词：Mist/steam cooling ; Internal ribbed channel ; Heat transfer enhancement ; Elevated operational conditions

刊名：International Journal of Heat and Mass Transfer

出版年：2017

5.Heat transfer in a two-inlet rotating wedge-shaped channel with various locations of the second inlet

作者：Hongwu Deng^a ; ^{denghw@buaa.edu.cn} ; Yancun Cheng^a ; ^{chengyancun@buaa.edu.cn} ; Yang Li^a ; ^{buaalzw@126.com} ; Bin Ni^b ; ^{mechanist@126.com} ; Lu Qiu^a ; ^{qiulu@buaa.edu.cn}

关键词：Gas turbine heat transfer ; Rotor blades trailing edge ; Rotating ; Multiple inlets

刊名：International Journal of Heat and Mass Transfer

出版年：2017

6.Heat transfer in a two-inlet rotating rectangular channel with side-wall fluid extraction

作者：Hongwu Deng ^{denghw@buaa.edu.cn" class="auth_mail" title="E-mail the corresponding author} ; Yanan Chen ^{chenyanan@buaa.edu.cn" class="auth_mail" title="E-mail the corresponding author} ; Zhi Tao ^{tao_zhi@buaa.edu.cn" class="auth_mail" title="E-mail the corresponding author} ; Yang Li ^{buaalzw@126.com" class="auth_mail" title="E-mail the corresponding author} ; Lu Qiu ; ^{qiulu@buaa.edu.cn" class="auth_mail" title="E-mail the corresponding author}

关键词：Gas turbine heat transfer ; Rotor blade trailing edge ; Rotating ; Counteracting flow

刊名：International Journal of Heat and Mass Transfer

出版年：2017

7.Local heat and mass transfer measurements for multi-layered impingement/effusion cooling: Effects of pin spacing on the impingement and effusion plate

作者：Seon Ho Kim^a ; ^{rcdkim@yonsei.ac.kr" class="auth_mail" title="E-mail the corresponding author} ; Kyeong Hwan Ahn^b ; ^{anhwan@hanmail.net" class="auth_mail" title="E-mail the corresponding author} ; Jun Su Park^c ; ^{js_park@ut.ac.kr" class="auth_mail" title="E-mail the corresponding author} ; Eui Yeop Jung^a ; ^{yobgi1004@yonsei.ac.kr" class="auth_mail" title="E-mail the corresponding author} ; Ki-Young Hwang^d ; ^{kiyhwang@naver.com" class="auth_mail" title="E-mail the corresponding author} ; Hyung Hee Cho^a ; ^{hhcho@yonsei.ac.kr" class="auth_mail" title="E-mail the corresponding author}

关键词：Heat and mass transfer ; Gas turbine ; Multi-layered impingement/effusion cooling ; Quasi-transpiration cooling

刊名：International Journal of Heat and Mass Transfer

出版年：2017

8.Thermo-structural analysis of cracks on gas turbine vane segment having multiple airfoils

作者：Heeyoon Chung^a ; Ho-Seong Sohn^a ; Jun Su Park^b ; Kyung Min Kim^c ; Hyung Hee Cho^a ; ^{hhcho@yonsei.ac.kr}

关键词：Gas turbine ; Nozzle vane segment ; Thermo-structural analysis ; Conjugate heat transfer ; Thermal stress

刊名：Energy

出版年：2017

9.Investigations of film cooling and heat transfer on a turbine blade squealer tip

作者：Kun He ^{hekun@mail.xjtu.edu.cn" class="auth_mail" title="E-mail the corresponding author}

关键词：Gas turbine ; Squealer tip ; Heat transfer ; Film cooling

刊名：Applied Thermal Engineering

出版年：2017

10.An investigation on an anti-ice static vane of a gas turbine engine

作者：Volkan Tatar^a ; ^{volkan.tatar@tei.com.tr" class="auth_mail" title="E-mail the corresponding author} ; Haydar Aras^b

关键词：Anti-ice system of gas turbine engine ; Icing ; Heat transfer analysis ; Flow visualization

刊名：Applied Thermal Engineering

出版年：2017

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