Optics and Precision Engineering, Volume. 26, Issue 8, 1888(2018)

Measurement of flow flux for scramjet isolator inflow based on absorption spectroscopy

XU Chao1... WANG Liao2, ZHONG Chen-guang2, KAN Rui-feng3 and XU Zhen-yu3 |Show fewer author(s)
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  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    References(14)

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    [2] [2] SONG W Y, MA X F, LIU W X, et al. Investigation on start performance of scramjet inlet[J]. Chinese Space Science and Technology, 2006, 26(6): 62-68.(in Chinese)

    [3] [3] LYLE K, JEFFRIES J, HANSON R, et al.. Aeroengine mass flux sensor based on laser absorption measurements of oxygen velocity and density[C].41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Tucson: AIAA,2005: 2005-3784.

    [4] [4] SONG J L, HONG Y J, WANG G Y, et al.. Simulation of mass flux measurement based on tunable diode laser absorption spectroscopy in non-uniform flows[J]. Optik - International Journal for Light and Electron Optics, 2013, 124(22): 5742-5746.

    [5] [5] O'BYRNE S, WITTIG S, KURTZ J, et al.. Diode laser sensor for scramjet inlets: final year report[S]. Program 2011. AOARD-104075.

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    [7] [7] MICHAEL B,TODD B. Post-flight analysis of the diode-laser-based mass capture experiment onboard HIFiRE flight 1[C]. 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco: AIAA,2011: 2011-2359.

    [8] [8] XU Z Y, KAN R F, RUAN J, et al.. A tunable diode laser absorption based velocity sensor for local field in hypersonic flows[C]. Optics and Photonics for Energy and the Environment, Optical Society of America, Leipzig,German, 2016, ETu2A.4.

    [10] [10] MILLER M F, KESSLER W J, ALLEN M G. Diode laser-based air mass flux sensor for subsonic aeropropulsion inlets[J].Applied Optics,1996, 35 (24): 4905-4912.

    [11] [11] LI F, YU X L, CAI W W, et al.. Uncertainty in velocity measurement based on diode laser absorption in nonuniform flows[J]. Appl. Opt., 2012,51(20): 4788-4797.

    [12] [12] JIA L Q, LIU W Q, KAN R F, et al.. Oxygen mass flow detection method in supersonic flow based on TDLAS[J]. Acta Photonica Sinica, 2015, 44(7) : 67-72.(in Chinese)

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    [14] [14] YAO L, LIU W Q, KAN R F, et al.. Research and development of a compact TDLAS system to measure scramjet combustion temperature[J]. Journal of Experiments in Fluid Mechanics, 2015, 29(1): 71-76.(in Chinese)

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    XU Chao, WANG Liao, ZHONG Chen-guang, KAN Rui-feng, XU Zhen-yu. Measurement of flow flux for scramjet isolator inflow based on absorption spectroscopy[J]. Optics and Precision Engineering, 2018, 26(8): 1888

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    Paper Information

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    Received: May. 9, 2018

    Accepted: --

    Published Online: Oct. 2, 2018

    The Author Email:

    DOI:10.3788/ope.20182608.1888

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