Search Results - "TL780 Rockets"

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  1. 1
    Study of effect of flow parameters on base pressure in a suddenly expanded duct at supersonic mach number regimes using CFD and design of experiments

    Study of effect of flow parameters on base pressure in a suddenly expanded duct at supersonic mach number regimes using CFD and design of experiments by Quadros, Jaimon Dennis, Khan, Sher Afghan, A. J., Antony

    Published 2018
    Subjects: “…TL780 Rockets…”
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  2. 2
    Base pressure behaviour in a suddenly expanded duct at supersonic mach number regimes using Taguchi design of experiments

    Base pressure behaviour in a suddenly expanded duct at supersonic mach number regimes using Taguchi design of experiments by Quadros, Jaimon Dennis, Khan, Sher Afghan, Antony, A J

    Published 2018
    Subjects: “…TL780 Rockets…”
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  3. 3
    Influence of expansion level on base pressure and reattachment length

    Influence of expansion level on base pressure and reattachment length by Pathan, Khizar Ahmed, Dabeer, Prakash S, Khan, Sher Afghan

    Published 2019
    Subjects: “…TL780 Rockets…”
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  4. 4
    Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for mach 3.0 using CFD.

    Experimental and numerical studies on flow from axisymmetric nozzle flow with sudden expansion for mach 3.0 using CFD. by Quadros, Jaimon Dennis, Khan, Sher Afghan, Antony, A J, S.Vas, Jolene

    Published 2016
    Subjects: “…TL780 Rockets…”
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  5. 5
    Active control of base pressure in suddenly expanded flow for area ratio 4.84

    Active control of base pressure in suddenly expanded flow for area ratio 4.84 by Ali Baig, Maughal Ahmed, Khan, Sher Afghan, Rathakrishnan, Ethirajan

    Published 2012
    Subjects: “…TL780 Rockets…”
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  6. 6
    Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25

    Studies on flow from converging nozzle and the effect of nozzle pressure ratio for area ratio of 6.25 by Ashfaq, Syed, Khan, Sher Afghan

    Published 2014
    Subjects: “…TL780 Rockets…”
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  7. 7
    Influence of micro jets on wall pressure for area ratio 3.24

    Influence of micro jets on wall pressure for area ratio 3.24 by Ashfaq, Syed, Khan, Sher Afghan

    Published 2014
    Subjects: “…TL780 Rockets…”
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  8. 8
    Active control of wall pressure flow field at low supersonic Mach numbers

    Active control of wall pressure flow field at low supersonic Mach numbers by Asad Ullah, Mohammed, Bashir, Musavir, Janvekar, Ayub, Khan, Sher Afghan

    Published 2016
    Subjects: “…TL780 Rockets…”
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  9. 9
    Pressure and its derivative with respect to piston Mach number for an oscillating cone

    Pressure and its derivative with respect to piston Mach number for an oscillating cone by Shabana, Ayesha, Monis, Renita, Crasta, Asha, Khan, Sher Afghan

    Published 2016
    Subjects: “…TL780 Rockets…”
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  10. 10
    Effect of nozzle pressure ratio and control jets location to control base pressure in suddenly expanded flows

    Effect of nozzle pressure ratio and control jets location to control base pressure in suddenly expanded flows by Pathan, Khizer Ahmed, Dabeer, Prakash S, Khan, Sher Afghan

    Published 2019
    Subjects: “…TL780 Rockets…”
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  11. 11
    Experimental research on wall pressure distribution in C-D nozzle at Mach number 1.1 for area ratio 3.24

    Experimental research on wall pressure distribution in C-D nozzle at Mach number 1.1 for area ratio 3.24 by Khan, Sher Afghan, Mokashi, Imran, Aabid, Abdul, Faheem, Mohammad

    Published 2019
    Subjects: “…TL780 Rockets…”
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  12. 12
    Influence of control mechanism on the flow field of duct at Mach 1.2 for area ratio 2.56

    Influence of control mechanism on the flow field of duct at Mach 1.2 for area ratio 2.56 by Khan, Sher Afghan, Aabid, Abdul, Chaudhary, Zakir Ilahi

    Published 2019
    Subjects: “…TL780 Rockets…”
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  13. 13
    Experimental research on flow development and control effectiveness in the duct at high speed

    Experimental research on flow development and control effectiveness in the duct at high speed by Khan, Sher Afghan, Ahmad, Zaheer, Aabid, Abdul, Mokashi, Imran

    Published 2019
    Subjects: “…TL780 Rockets…”
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  14. 14
    A cost-effective data acquisition instrumentation for measurement of base pressure and wall pressure in suddenly expanded flow through ducts

    A cost-effective data acquisition instrumentation for measurement of base pressure and wall pressure in suddenly expanded flow through ducts by Sethuraman, Vigneshvaran, Rajendran, Parvathy, Khan, Sher Afghan

    Published 2019
    Subjects: “…TL780 Rockets…”
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  15. 15
    Investigation of base flow for an axisymmetric suddenly expanded nozzle with micro JET

    Investigation of base flow for an axisymmetric suddenly expanded nozzle with micro JET by Chaudhary, Zakir Ilahi, Shinde, Vilas B., Khan, Sher Afghan

    Published 2018
    Subjects: “…TL780 Rockets…”
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  16. 16
    Enlarge duct length optimization for suddenly expanded flows

    Enlarge duct length optimization for suddenly expanded flows by Pathan, Khizer Ahmed, Dabeer, Prakash S, Khan, Sher Afghan

    Published 2020
    Subjects: “…TL780 Rockets…”
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  17. 17
    An investigation of effect of control jets location and blowing pressure ratio to control base pressure in suddenly expanded flows

    An investigation of effect of control jets location and blowing pressure ratio to control base pressure in suddenly expanded flows by Pathan, Khizar Ahmed, Dabeer, Prakash S, Khan, Sher Afghan

    Published 2020
    Subjects: “…TL780 Rockets…”
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  18. 18
    Analysis of parameters affecting thrust and base pressure in suddenly expanded flow from nozzle

    Analysis of parameters affecting thrust and base pressure in suddenly expanded flow from nozzle by Pathan, Khizar Ahmed, Syed, Ashfaq, Dabeer, Prakash S, Khan, Sher Afghan

    Published 2019
    Subjects: “…TL780 Rockets…”
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  19. 19
    Numerical investigation of splitter plate effect on the bluff body using finite volume method

    Numerical investigation of splitter plate effect on the bluff body using finite volume method by Afifi, Azmil, Aabid, Abdul, Khan, Sher Afghan

    Published 2020
    Subjects: “…TL780 Rockets…”
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  20. 20
    Comparing the effect of different turbulence models on the CFD predictions of NACA0018 airfoil aerodynamics

    Comparing the effect of different turbulence models on the CFD predictions of NACA0018 airfoil aerodynamics by Khan, Sher Afghan, Bashir, Musavir, Baig, Maugal Ahmed Ali, Mehaboob Ali, Fharukh Ahmed Ghasi

    Published 2020
    Subjects: “…TL780 Rockets…”
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