Two quantitative schlieren methods are assessed and compared: calibrated color schlieren (CCS) and background oriented schlieren (BOS). Both methods are capable of measuring the light deflection angle in two spatial directions, and hence the projected density gradient vector field. Spatial integration using the conjugate gradient method returns the projected density field. To assess the performance of CCS and BOS, density measurements of a two-dimensional benchmark flow (a Prandtl-Meyer expansion fan) are compared with the theoretical density field and with the density inferred from PIV velocity measurements. The method’s performance is also evaluated a priori from an experiment ray-tracing simulation. The density measurements show good agreement with theory. Moreover, CCS and BOS return comparable results with respect to each other and with respect to the PIV measurements. BOS proves to be very sensitive to displacements of the wind tunnel during the experiment and requires a correction for it, making it necessary to apply extra boundary conditions in the integration procedure. Furthermore, spatial resolution can be a limiting factor for accurate measurements using BOS. CCS suffers from relatively high noise in the density gradient measurement due to camera noise and has a smaller dynamic range when compared to BOS. Finally the application of the two schlieren methods to a separated wake flow is demonstrated. Flow features such as shear layers and expansion and recompression waves are measured with both methods.
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COMOTI, Romanian Res & Developing Inst Gas Turbines, Bucharest 061126, RomaniaCOMOTI, Romanian Res & Developing Inst Gas Turbines, Bucharest 061126, Romania
Prisacariu, Emilia Georgiana
Prisecaru, Tudor
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Univ Politehn Bucuresti, Fac Mech Engn & Mechatron, Bucharest 060042, RomaniaCOMOTI, Romanian Res & Developing Inst Gas Turbines, Bucharest 061126, Romania
Prisecaru, Tudor
Dombrovschi, Madalin Constantin
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COMOTI, Romanian Res & Developing Inst Gas Turbines, Bucharest 061126, RomaniaCOMOTI, Romanian Res & Developing Inst Gas Turbines, Bucharest 061126, Romania
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Lund Univ, Dept Energy Sci, Div Heat Transfer, Lund, Sweden
Karman Inst Fluid Dynam, Dept Turbomachinery & Prop, Rhode St Genese, BelgiumLund Univ, Dept Energy Sci, Div Heat Transfer, Lund, Sweden
Cakir, Bora O.
Sanned, David
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Lund Univ, Dept Phys, Div Combust Phys, Lund, SwedenLund Univ, Dept Energy Sci, Div Heat Transfer, Lund, Sweden
Sanned, David
Prakash, Megha
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Lund Univ, Dept Phys, Div Combust Phys, Lund, SwedenLund Univ, Dept Energy Sci, Div Heat Transfer, Lund, Sweden
Prakash, Megha
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Brackmann, Christian
Richter, Mattias
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Lund Univ, Dept Phys, Div Combust Phys, Lund, SwedenLund Univ, Dept Energy Sci, Div Heat Transfer, Lund, Sweden
Richter, Mattias
Fureby, Christer
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Lund Univ, Dept Energy Sci, Div Heat Transfer, Lund, SwedenLund Univ, Dept Energy Sci, Div Heat Transfer, Lund, Sweden