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会议文集


文集名Heat Transfer: Combustors; Heat Transfer: Film Cooling
会议名2024 ASME Turbo Expo: Turbomachinery Technical Conference and Exposition (GT 2024)
中译名《2024年ASME涡轮机博览会：涡轮机技术会议与展览会，卷7》
机构American Society of Mechanical Engineers (ASME)
会议日期24-28 June 2024
会议地点London, UK
出版年2024
馆藏号354047


题名作者出版年
A REVIEW OF SECONDARY COMBUSTION ON TURBINE BLADE COOLINGTinashe Ngwenya; Antonino Nava; Peter T. Ireland2024
EFFECTS OF CURVATURE AND COMPOUND ANGLE ON COOLING PERFORMANCE AND FLOW CHARACTERISTICS FOR A COMBUSTOR LINER WITH TANGENTIAL EFFUSION COOLING CONFIGURATIONXuanwu Chen; Min Yao; Qinghua Zeng; Ziwan Li; Pengfu Xie2024
Overall Cooling Effectiveness of Effusion Cooled and Thermal Barrier Coated Swirl Stabilized Liquid Fueled Combustor Liner in Reacting Flow Conditions With Infrared ThermographyIbrahim Edhem Tin; Muhammed Emin Ural; Hamdullah Ozogul2024
EFFUSION COOLING CHARACTERISTICS OF EFFUSION-COOLED COMBUSTOR LINERS WITH DIFFERENT HOLE CONFIGURATIONS UNDER SWIRL IMPACTXiang Lu; Yuliang Jia; Yongbin Ji; Bing Ge; Shusheng Zang2024
LES INVESTIGATION OF FILM COOLING IN ROTATING DETONATION COMBUSTORS Shreyas Ramanagar Sridhara.~1, Antonio Andreini~1, Marc D. Polanka~2, Myles D. Bohon~3Shreyas Ramanagar Sridhara; Antonio Andreini; Marc D. Polanka; Myles D. Bohon2024
INFLUENCE OF DILUTION AND EFFUSION FLOWS IN GENERATING VARIABLE INLET PROFILES FOR A HIGH-PRESSURE TURBINEChad B. Schaeffer; Michael D. Barringer; Stephen P. Lynch; Karen A. Thole2024
DIRT INGESTION IMPACTS ON COOLING WITHIN A DOUBLE-WALLED COMBUSTOR LINERKyle McFerran; Karen A. Thole; Stephen P. Lynch2024
INVESTIGATION OF HOT STREAK MIGRATIONS IN A TRIPLE DUAL-STAGE SWIRLER COMBUSTOR COUPLED WITH TURBINE VANES UNDER DIFFERENT CONTRACTION RATIOSJiacheng Lyu; Keqi Hu; Zhixin Zhu; Gaofeng Wang2024
RESEARCH ON FILM COOLING CHARACTERISTICS AND MECHANISM OF LONGITUDINAL CORRUGATED HEAT SHIELD IN AFTERBURNERSong Fu; Cun-liang Liu; Hai-yong Liu; Zi-wen Wang; Xiao-hui Bai2024
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF THE INCLINATION ANGLE EFFECT ON THE COOLING EFFECTIVENESS IN A LIQUID FUELED CAN TYPE COMBUSTORGamze Gulenc; Hamdullah Ozogul2024
ASSESSMENT OF A SIMPLIFIED CONJUGATE HEAT TRANSFER PERFORATED WALL MODEL FOR THE EFFUSION COOLING BY LES METHODMengming Wang; Chenzhen Ji; Shikang Lu; Wentao Shi; Tong Zhu2024
WALL-MODELED LARGE EDDY SIMULATION AND CONJUGATE HEAT TRANSFER FOR COMBUSTOR AEROTHERMAL APPLICATIONSNaseem Ansari; Carlo Arguinzoni; Stefano Orsino; Reza Farokhi; Ishan Verma2024
SUPERPOSITION OF OVERALL COOLING EFFECTIVENESS ON A TURBINE BLADE LEADING EDGEBailey W. Hopkins; James L. Rutledge2024
FILM COOLING PERFORMANCE ON ROTATING BLADE LEADING EDGE WITH VARIOUS ROTATING SPEED AND FILM HOLE STRUCTURESYan Jiang; Yi Huang; Haiwang Li; Zhiyu Zhou; Gang Xie2024
EFFECT OF BLOCKAGES ON FILM EFFECTIVENESS ON THE PRESSURE SURFACE OF A TURBINE BLADETassilo von Mueller; David Bacci; Augustin Wambersie; Holt Wong; Peter Ireland; Dougal Jackson2024
ENHANCED ADIABATIC FILM COOLING EFFECTIVENESS BY VARYING COMPOUND ANGLEYeongmin Pyo; Patrick Richer; Mohsen Broumand; Bertrand Jodoin; Juchan Son; Zekai Hong2024
EFFECT OF THE UPSTREAM SHROUD PURGE FLOW ON THE COOLING PERFORMANCES OF TURBINE BLADE TIPZhenzhen Xue; Haiwang Li; Zhi Tao; Zhiyu Zhou; Long Meng; Gang Xie2024
A COMBINED LES AND PIV INVESTIGATION OF TRENCHED FAN-SHAPED HOLE AERODYNAMICSG. Barigozzi; A. Zamiri; S. Gamba; I. Spozio; J. T. Chung2024
GEOMETRIC AND FLOW CHARACTERIZATION OF ADDITIVELY MANUFACTURED TURBINE BLADES WITH DRILLED FILM COOLING HOLESKelsey E. McCormack; Maria Rozman; Reid A. Berdanier; Karen A. Thole2024
EFFECT OF RELATIVE LOCATION OF FILM COOLING HOLE WITH INTERNAL ANGLED RIBS ON THE FILM COOLING EFFECTIVENESS OF A GAS TURBINE BLADEYoung Jun Kang; Jin Young Jeong; Hyeok Je Kim; Gi Mun Kim; Jae Su Kwak2024
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