Brummund, U. and Mesnier, B. (1999) Experimental Study of Compressible Mixing Layers. In: Fourteenth International Symposium on Air Breathing Engines. AIAA. 14th International Symposium on Airbreathing Engines, Florence, Sept. 5-10, 1999. ISBN 1-56347-357-7.
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An experimental investigation of the mixing process of a compressible shear/mixing layer in a supersonic model combustion chamber has been performed by applying laser based optical diagnostics like planar Rayleigh and Mie scattering. The influence of compressibility on the mixing layer has been analyzed, confirming that the mixing layer growth rate is decreasing with increasing compressibility. Furthermore the interaction between a shock wave and the shear/mixing layer was studied as a test case for shear layer growth rate enhancement. A slight but significant shear layer growth rate enhancement can be achieved by shock wave / mixing layer interaction.
|Document Type:||Conference or Workshop Item (Paper)|
|Additional Information:||LIDO-Berichtsjahr=1999, monograph_id=ISABE 99-7131,|
|Title:||Experimental Study of Compressible Mixing Layers.|
|Journal or Publication Title:||Fourteenth International Symposium on Air Breathing Engines|
|Event Title:||14th International Symposium on Airbreathing Engines, Florence, Sept. 5-10, 1999|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Space (old)|
|HGF - Program Themes:||W RP - Raumtransport|
|DLR - Research area:||Space|
|DLR - Program:||W RP - Raumtransport|
|DLR - Research theme (Project):||E -- no assignement|
|Institutes and Institutions:||Institute of Space Propulsion|
|Deposited By:||Monika Lohmiller|
|Deposited On:||16 Sep 2005|
|Last Modified:||06 Jan 2010 12:39|
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