• DocumentCode
    2771792
  • Title

    A combined holographic interferometer and laser-schlieren system applied to high temperature, high velocity flows

  • Author

    Kastell, Dirk ; Eitelberg, Georg

  • Author_Institution
    Deutsche Forschungsanstalt fur Luft- und Raumfahrt, Gottingen, Germany
  • fYear
    1995
  • fDate
    18-21 Jul 1995
  • Firstpage
    42705
  • Lastpage
    42711
  • Abstract
    The High Enthalpy tunnel in Gottingen (HEG) is operated by the German Aerospace Research Establishment (DLR). Nominal test conditions of a free stream Mach number of 10, reservoir enthalpies of up to 23 MJ/kg and reservoir pressures of up to 100 MPa make the HEG ideal to study the “hot” entry phase of space vehicles. For the flow visualisation in the HEG a holographic interferometer with a 300 mm field of view is set-up. It uses the phase step technique for the evaluation of the holograms. This method enables computerized evaluation of the holograms to create high quality interferograms by increasing the signal to noise ratio. Complete flow field density gradients around two dimensional models can be calculated from the interferograms. Nevertheless for three dimensional models, where the integration length of the light path is too short to obtain a large fringe shift, the exact localisation of the shocks is difficult. To overcome this lack of the holographic interferometric system it has been extended by a laser-schlieren system to obtain simultaneous interferometric and schlieren information. Results that are presented for the hyperboloid flare model demonstrate the feasibility of the combined system. A comparison of laser-schlieren and hologram-schlieren images made for the axisymmetric Electre model show that the resolution of a direct recorded schlieren image is much higher than the latter
  • Keywords
    aerodynamics; aerospace testing; flow measurement; flow visualisation; holographic interferometry; hypersonic flow; measurement by laser beam; schlieren systems; wind tunnels; 100 MPa; axisymmetric Electre model; direct recorded schlieren image; entry phase; exact localisation; flow field density gradients; flow visualisation; free stream Mach number; high enthalpy tunnel; high velocity flows; holographic interferometer; hyperboloid flare model; laser-schlieren system; phase step technique; reservoir enthalpies; reservoir pressures; signal to noise ratio; space vehicles; three dimensional models; Aerospace testing; Electric shock; Holography; Image resolution; Laser modes; Optical interferometry; Reservoirs; Signal to noise ratio; Space vehicles; Visualization;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Instrumentation in Aerospace Simulation Facilities, 1995. ICIASF '95 Record., International Congress on
  • Conference_Location
    Wright-Patterson AFB, OH
  • Print_ISBN
    0-7803-2088-3
  • Type

    conf

  • DOI
    10.1109/ICIASF.1995.519118
  • Filename
    519118