Showing 321 - 340 results of 849 for search '"combustion"', query time: 0.06s Refine Results
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    Industrial Furnaces in Problem of Nitrogen Oxide Emission Reduction by B. S. Soroka

    Published 2004-08-01
    “…The paper analyzes methods of reducing nitrogen oxide emission in industrial furnace combustion products. Special attention is given to techniques of emission reduction while organizing low-emission fuel combustion. …”
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    Article
  9. 329

    Statistical Analysis of Flame Oscillation Characterization of Oxy-Fuel in Heavy Oil Boiler Using OH Planar Laser-Induced Fluorescence by Xin Yu, Zhen Cao, JiangBo Peng, Yang Yu, Guang Chang, Yufei Ma, XiaoHui Li, Chaobo Yang, ZhiQiang Wang

    Published 2019-01-01
    “…Combustion instabilities, such as flame oscillation and combustion fluctuation, can assess the performance of an industrial burner in the boiler. …”
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  10. 330

    A Model for Igniter Mass Flow Rate History Evaluation for Solid Rocket Motors by Yanjie Ma, Futing Bao, Weihua Hui, Yang Liu, Yijie Gao

    Published 2019-01-01
    “…The coupling between the flow field variables in the combustion chamber and the heat transfer at the gas-solid interface is computed in a segment way. …”
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    Article
  11. 331

    STUDYING HOW DIESEL ENGINE ADDITIVES USING SILVER OXIDE (Ag2O) NANOPARTICLES AFFECT THE ENVIRONMENT by CIHAN BAYINDIRLI, MEHMET CELIK

    Published 2024-07-01
    “…Due to the improvement in the combustion reaction, CO2 emission increased with product of complete combustion. …”
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    Article
  12. 332

    A Novel Segmentation Method for Furnace Flame Using Adaptive Color Model and Hybrid-Coded HLO by Pinggai Zhang, Minrui Fei, Ling Wang, Xian Wu, Chen Peng, Kai Chen

    Published 2021-01-01
    “…In recent years, the combustion furnace has been widely applied in many different fields of industrial technology, and the accurate detection of combustion states can effectively help operators adjust combustion strategies to improve combustion utilization and ensure safe operation. …”
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  13. 333
  14. 334

    The Oxygen Generation Performance of Hollow-Structured Oxygen Candle for Refuge Space by Weixiang Wang, Longzhe Jin, Na Gao, Jianlin Wang, Mingyang Liu

    Published 2018-01-01
    “…The oxygen generation rate (OGR) and other properties were explored by combustion experiments. The composition of the oxygen candles and the residual solids after combustion were observed with scanning electron microscope (SEM). …”
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  15. 335

    Analytical Equations for Thermoacoustic Instability Sources and Acoustic Radiation from Reacting Turbulence by S. A. E. Miller

    Published 2020-01-01
    “…A series of solutions are presented via the method of the vector Green’s function. We identify both combustion-combustion and combustion-aerodynamic interaction source terms. …”
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    Peculiar Features of Burning Alternative Motor Fuels by M. Assad, O. G. Penyazkov

    Published 2006-04-01
    “…Some peculiar features of air-hydrogen mixture combustion process in a modeling combustion chamber are given in the paper. …”
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  18. 338

    Experimental Study of Methods of Increasing the Efficiency of a Direct-Flow Air-Jet Detonation Engine by Vitalii Stoliarchuk, Oleksandr Zolotko, Oleksandr Aksonov

    Published 2023-06-01
    “…The use of detonation fuel combustion allows to increase the thermodynamic efficiency of the engine and the thermodynamic efficiency of fuel combustion. …”
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  19. 339

    Burning Rate Enhancement Analysis of End-Burning Solid Propellant Grains Based on X-Ray Real-Time Radiography by Wei Xianggeng, Bo Tao, Wang Pengbo, Ma Xinjian, Lou Yongchun, Chen Jian

    Published 2020-01-01
    “…It is generally believed that this phenomenon is caused by the nonparallel layer combustion of the burning surface, resulting in the increase of burning rate along the inhibitor. …”
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  20. 340

    Investigations on Internal Ballistic Characteristics of Pasty Propellant Rocket Engine by Xinyou Shan, Yingkun Li, Xiong Chen, Yan Wu, Yong He, Weixuan Li

    Published 2021-01-01
    “…The transport pipe diameter changes from 11.3 mm to 7.4 mm, and the initial combustion time and residual propellant combustion time decreased by 41.3% and 36.0%. …”
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    Article