Synonyme wurden verwendet für: Turbine
Suche ohne Synonyme: keywords:("Turbine")

1–20 von 7,722 Ergebnissen
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    Design methodology for combustor in advanced gas turbine engines: a review

    Kim, Insong / Jin, Hakson / Ri, Kwangsong et al. | Emerald Group Publishing | 2024
    Schlagwörter: Gas turbine engine

    Improving the Accuracy of Performance Calculation for Multistage Axial Turbines of Aircraft Engines Using Three-Dimensional Numerical Modeling

    Popov, G. M. / Zubanov, V. M. / Goryachkin, E. S. et al. | Springer Verlag | 2024
    Schlagwörter: gas turbine engine , multistage turbine

    Principles of turbomachinery in air-breathing engines

    Baskharone, Erian A. / Hill, D. Lee | TIBKAT | 2024
    Schlagwörter: Gas-turbines

      Principles of turbomachinery in air-breathing engines

      Baskharone, Erian A. | SLUB | 2006
      Schlagwörter: Gas-turbines

    Modelling width of the spectral component of a gas-turbine engine gearbox output shaft speed

    Freier Zugriff
    A. E. Sundukov / E. V. Shakhmatov | DOAJ | 2024
    Schlagwörter: gas-turbine engine

    Analysis of systems for cooling liquid injection in turbine engine gas flow duct

    Freier Zugriff
    Ruslan Tsukanov / Sergii Yepifanov | DOAJ | 2024
    Schlagwörter: gas-turbine engine

    Advanced wind turbines

    MohanKumar, Palanisamy / Sivalingam, Krishnamoorthi / Lim, Teik-Cheng | TIBKAT | 2024
    Schlagwörter: Wind turbines

    Analysis of environmentally friendly commercial aviation development ways

    Freier Zugriff
    Ruslan Tsukanov / Sergii Yepifanov | DOAJ | 2024
    Schlagwörter: gas-turbine engine

    Hot Corrosion Damage Modeling in Aeroengines Based on Performance and Flight Mission

    Pontika, Evangelia / Laskaridis, Panagiotis / Nikolaidis, Theoklis et al. | AIAA | 2024
    Schlagwörter: Gas Turbine Engines , Gas Turbine Performance

    Secondary flows and losses in radial turbine volutes

    Li, Chao / Chen, Hua / Wang, Yu et al. | SAGE Publications | 2024
    Schlagwörter: Radial turbine

    Research on modeling method of non-axisymmetric endwall based on body-fitted coordinates

    Wang, Zhiguo / Wang, Pei / Liu, Jun et al. | SAGE Publications | 2024
    Schlagwörter: gas turbine

    Application of LCA to Aviation

    Çalışır, D. / Ekici, Selçuk / Midilli, A. et al. | Springer Verlag | 2024
    Schlagwörter: Gas turbine engine

    Experimental investigation on the aerodynamic performance of a transonic turbine rotor with non-axisymmetric endwall

    Wang, Jie / Yan, Yifei / Tao, Zhi et al. | Elsevier | 2024
    Schlagwörter: Transonic turbine

    Influence of nonuniform velocity and temperature inlet on the mixing characteristics of a TBCC multibypass combustor with a double-mixer configuration

    Zhao, Wensheng / Fan, Weijun / Zhang, Rongchun | Elsevier | 2024
    Schlagwörter: Turbine-based combined engine

    Adaptive positioning technology of film cooling holes in hollow turbine blades

    Huang, Wangwang / Mei, Xuesong / Fan, Zhengjie et al. | Elsevier | 2024
    Schlagwörter: Hollow turbine blades

    Numerical investigation of boundary layer separation control on the low-pressure turbine blade by oscillatory blowing

    Yang, PengCheng / Chen, ShaoWen / Chen, ShuaiTong et al. | Elsevier | 2024
    Schlagwörter: Low pressure turbine

    A review of challenges and framework development for corrosion fatigue life assessment of monopile-supported horizontal-axis offshore wind turbines

    Freier Zugriff
    Okenyi, Victor / Bodaghi, Mahdi / Mansfield, Neil et al. | Taylor & Francis Verlag | 2024
    Schlagwörter: Offshore wind turbine

    Topology Optimization of 3D Turbine Disk Considering Thermal Load Based on BESO Method

    Meng, Zihao / Ren, Yiru / Ding, Chao et al. | ASCE | 2024
    Schlagwörter: Turbine disk

    Uncertainty quantification of geometric variations in transonic high-pressure turbine with different trailing edge and throat area distribution

    Chen, Yongchao / Zou, Zhengping / Yao, Lichao et al. | Elsevier | 2024
    Schlagwörter: Transonic high-pressure turbine