يعرض 1 - 20 نتائج من 49 نتيجة بحث عن '"Bao, Futing"', وقت الاستعلام: 0.51s تنقيح النتائج
  1. 1
    Academic Journal
    Mixing and combustion characteristics analysis for solid rocket ramjet

    المؤلفون: Lei, Xiaoyu, Sun, Lin, Cheng, Jiming, He, Desheng, Bao, Futing, Feng, Xiping

    المصدر: Journal of Physics: Conference Series ; volume 2472, issue 1, page 012014 ; ISSN 1742-6588 1742-6596

    الاتاحة: http://dx.doi.org/10.1088/1742-6596/2472/1/012014
    https://iopscience.iop.org/article/10.1088/1742-6596/2472/1/012014
    https://iopscience.iop.org/article/10.1088/1742-6596/2472/1/012014/pdf

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  2. 2
    Academic Journal
    Structural analysis of solid rocket motor with effects of viscoelastic Poisson's ratio

    المؤلفون: Wang, Junqi, Bao, Futing, Cui, Huiru

    المصدر: Journal of Physics: Conference Series ; volume 2285, issue 1, page 012020 ; ISSN 1742-6588 1742-6596

    الاتاحة: http://dx.doi.org/10.1088/1742-6596/2285/1/012020
    https://iopscience.iop.org/article/10.1088/1742-6596/2285/1/012020
    https://iopscience.iop.org/article/10.1088/1742-6596/2285/1/012020/pdf

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  3. 3
    Academic Journal
    Research on Oscillation Response of Pressure-Combustion-Thrust System in Solid Rocket Motor.

    المؤلفون: Li, Lu1 (AUTHOR) lilu_nwpu@mail.nwpu.edu.cn, Bao, Futing1 (AUTHOR) ftbao@nwpu.edu.cn, Wei, Ran2 (AUTHOR) weiran@nwpu.edu.cn, Hou, Kaiyu3 (AUTHOR) houkyno8@126.com, Shi, Xiaoming4 (AUTHOR) daybreakxmshi@126.com

    المصدر: Journal of Aerospace Engineering. Jul2024, Vol. 37 Issue 4, p1-12. 12p.

    مصطلحات موضوعية: *ROCKET engines, *OSCILLATIONS, *FLUCTUATIONS (Physics), *THRUST, *COUPLINGS (Gearing)


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  4. 4
    Academic Journal
    An efficient approach for computing the finite time Lyapunov exponent in complex three-dimensional flow based on the discrete phase model

    المؤلفون: Bian, Fang, Sun, Lin, Shi, Delei, Bao, Futing

    المصدر: Aerospace Science and Technology ; volume 133, page 108110 ; ISSN 1270-9638

    الاتاحة: http://dx.doi.org/10.1016/j.ast.2023.108110
    https://api.elsevier.com/content/article/PII:S127096382300007X?httpAccept=text/xml
    https://api.elsevier.com/content/article/PII:S127096382300007X?httpAccept=text/plain

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  5. 5
    Academic Journal
    Research on thermal contact resistance between C/C and resin thermal protection materials for solid rocket motor nozzles considering real surface roughness

    المؤلفون: Sun, Lin, Jia, Huiyin, Lei, Xiaoyu, Bao, Futing

    المساهمون: SAST, Natural Science Basic Research Program of Shaanxi Province

    المصدر: Tribology International ; volume 186, page 108626 ; ISSN 0301-679X

    الاتاحة: http://dx.doi.org/10.1016/j.triboint.2023.108626
    https://api.elsevier.com/content/article/PII:S0301679X23004140?httpAccept=text/xml
    https://api.elsevier.com/content/article/PII:S0301679X23004140?httpAccept=text/plain

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  6. 6
    Academic Journal
    Quantitative analysis of enhanced mixing and combustion by lobed mixer in a ramjet engine: Study using hyperbolic Lagrangian coherent structures

    المؤلفون: Sun, Lin, Bian, Fang, Lei, Xiaoyu, Shi, Delei, Bao, Futing

    المصدر: Aerospace Science and Technology ; volume 140, page 108471 ; ISSN 1270-9638

    الاتاحة: http://dx.doi.org/10.1016/j.ast.2023.108471
    https://api.elsevier.com/content/article/PII:S1270963823003681?httpAccept=text/xml
    https://api.elsevier.com/content/article/PII:S1270963823003681?httpAccept=text/plain

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  7. 7
    Academic Journal
    Study on mixing and combustion characteristics of solid rocket ramjet with a large angle of attack

    المؤلفون: Shi, Delei, Sun, Lin, Cheng, Jiming, Bao, Futing, Feng, Xiping

    المصدر: Aerospace Science and Technology ; volume 141, page 108534 ; ISSN 1270-9638

    الاتاحة: http://dx.doi.org/10.1016/j.ast.2023.108534
    https://api.elsevier.com/content/article/PII:S1270963823004315?httpAccept=text/xml
    https://api.elsevier.com/content/article/PII:S1270963823004315?httpAccept=text/plain

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  8. 8
    Book
    An automatic CFD program for the rocket nozzle

    المؤلفون: Ma, YanJie, Bao, FuTing, Hui, WeiHua

    المصدر: Advances in Energy Science and Equipment Engineering II ; page 1619-1622

    الاتاحة: http://dx.doi.org/10.1201/9781315116174-148
    http://www.crcnetbase.com/doi/pdf/10.1201/9781315116174-148

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  9. 9
    Book
    Optimization design of propellant grain’s shape parameters based on structural integrity analysis

    المؤلفون: Xu, Hao, Bao, Futing, Lin, Ze

    المصدر: Advances in Energy Science and Equipment Engineering II ; page 1099-1102

    الاتاحة: http://dx.doi.org/10.1201/9781315116174-49
    http://www.crcnetbase.com/doi/pdf/10.1201/9781315116174-49

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  10. 10
    Academic Journal
    Combined Acceleration Methods for Solid Rocket Motor Grain Burnback Simulation Based on the Level Set Method

    المؤلفون: Wei, Ran, Bao, Futing, Liu, Yang, Hui, Weihua

    المصدر: International Journal of Aerospace Engineering ; volume 2018, page 1-12 ; ISSN 1687-5966 1687-5974

    الاتاحة: http://dx.doi.org/10.1155/2018/4827810
    http://downloads.hindawi.com/journals/ijae/2018/4827810.pdf
    http://downloads.hindawi.com/journals/ijae/2018/4827810.xml

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  11. 11
    Academic Journal
    Erratum to “Combined Acceleration Methods for Solid Rocket Motor Grain Burnback Simulation Based on the Level Set Method”

    المؤلفون: Wei, Ran, Bao, Futing, Liu, Yang, Hui, Weihua

    المصدر: International Journal of Aerospace Engineering ; volume 2018, page 1-1 ; ISSN 1687-5966 1687-5974

    الاتاحة: http://dx.doi.org/10.1155/2018/2353607
    http://downloads.hindawi.com/journals/ijae/2018/2353607.pdf
    http://downloads.hindawi.com/journals/ijae/2018/2353607.xml

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  12. 12
    Academic Journal
    Numerical and experimental investigation on turbulent flow and secondary flow in a 180° bend -- Circular Cross-section

    المؤلفون: Shao, Qing, Hui, Weihua, Bao, Futing

    المصدر: IOP Conference Series: Earth and Environmental Science ; volume 189, page 022061 ; ISSN 1755-1315

    الاتاحة: http://dx.doi.org/10.1088/1755-1315/189/2/022061
    http://stacks.iop.org/1755-1315/189/i=2/a=022061/pdf
    http://stacks.iop.org/1755-1315/189/i=2/a=022061?key=crossref.b335a7270428579a1109499f8e3d019f

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  13. 13
    Conference
    Numerical Simulation of Ignition Transient for Solid Rocket Motors with Large Aspect Ratio

    المؤلفون: Ma, Yanjie, Zhan, Mingming, Bao, Futing, Sun, Lin, Wei, Ran

    المصدر: 2021 12th International Conference on Mechanical and Aerospace Engineering (ICMAE)

    الاتاحة: http://dx.doi.org/10.1109/icmae52228.2021.9522550
    http://xplorestaging.ieee.org/ielx7/9521959/9522363/09522550.pdf?arnumber=9522550

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  14. 14
    Conference
    Dynamic Identification of Nozzle Throat Diameter of a Solid Rocket Motor and Experimental Validation based on Micron-CT 3D Reconstruction

    المؤلفون: Sun, Lin, Yu, Chengbo, Zhao, Yu, Bao, Futing, Liu, Yang, Hui, Weihua

    المصدر: 2020 11th International Conference on Mechanical and Aerospace Engineering (ICMAE)

    الاتاحة: http://dx.doi.org/10.1109/icmae50897.2020.9178858
    http://xplorestaging.ieee.org/ielx7/9171913/9178848/09178858.pdf?arnumber=9178858

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  15. 15
    Academic Journal
    Research on Flow Characteristics of a Variable Mach Number Aerodynamic Test Device by a Rotating Profile.

    المؤلفون: Chen, Zaicheng, Liu, Yang, Bao, Futing, Wei, Ran

    المصدر: International Journal of Aerospace Engineering; 3/16/2022, p1-14, 14p

    مصطلحات موضوعية: MACH number, CUBIC curves, AERODYNAMICS, TESTING equipment, EVALUATION methodology

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  16. 16
    Academic Journal
    Coupled Thermo-Structural Analysis Model of Solid Rocket Motor Nozzle considering the Variation of Friction Coefficient under Operating Conditions.

    المؤلفون: Sun, Lin, Jia, Huiyin, Zhang, Nan, Zhao, Yu, Bao, Futing

    المصدر: International Journal of Aerospace Engineering; 2/21/2022, p1-17, 17p

    مصطلحات موضوعية: ROCKET engines, FRICTION, NOZZLES, FIRE testing, SOLID propellant rockets, THERMAL resistance

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  17. 17
    Conference
    Solving Level Set Evolving Using Fully Convolution Network

    المؤلفون: Wei, Ran, Bao, Futing, Liu, Yang, Hui, Weihua

    المصدر: 2017 9th International Conference on Intelligent Human-Machine Systems and Cybernetics (IHMSC) ; volume 89, page 234-238

    الاتاحة: http://dx.doi.org/10.1109/ihmsc.2017.61
    http://xplorestaging.ieee.org/ielx7/8046763/8047557/08047620.pdf?arnumber=8047620

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  18. 18
    Conference
    Clustering Analysis on Internal Flow Field of a Spinning Solid Rocket Motor Nozzle

    المؤلفون: Sun, Lin, Bao, Futing, Hui, Weihua, Liu, Yang, Sui, Jiuling

    المصدر: 2017 9th International Conference on Intelligent Human-Machine Systems and Cybernetics (IHMSC) ; volume 29, page 121-124

    الاتاحة: http://dx.doi.org/10.1109/ihmsc.2017.34
    http://xplorestaging.ieee.org/ielx7/8046763/8047557/08047593.pdf?arnumber=8047593

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  19. 19
    Academic Journal
    A New Erosive Burning Model of Solid Propellant Based on Heat Transfer Equilibrium at Propellant Surface.

    المؤلفون: Ma, Yanjie1 (AUTHOR), Bao, Futing1 (AUTHOR), Sun, Lin1 (AUTHOR), Liu, Yang1 (AUTHOR), Hui, Weihua1 (AUTHOR)

    المصدر: International Journal of Aerospace Engineering. 12/16/2020, p1-9. 9p.

    مصطلحات موضوعية: *PROPELLANTS, *SOLID propellants, *HEAT transfer, *HEAT transfer coefficient, *ROCKET engines, *HEAT flux

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  20. 20
    Academic Journal
    Crack cause analysis of a graphite nozzle throat insert

    المؤلفون: Sun, Lin, Bao, Futing, Zhao, Yu, Hou, Lian, Hui, Weihua, Zhang, Ning, Shi, Wei

    المساهمون: National Natural Science Foundation of China, Aerospace Innovation Foundation

    المصدر: Acta Astronautica ; volume 137, page 70-77 ; ISSN 0094-5765

    الاتاحة: http://dx.doi.org/10.1016/j.actaastro.2017.04.016
    https://api.elsevier.com/content/article/PII:S0094576516313881?httpAccept=text/xml
    https://api.elsevier.com/content/article/PII:S0094576516313881?httpAccept=text/plain

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