Kost, F. and Gieß, P.-A. (2004) Experimental Turbine Research at DLR Göttingen. Journal of the Gas Turbine Society of Japan, Vol. 32 (No. 6), pp. 47-56.
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At DLR Goettingen (Germany) two windtunnels especially adapted to turbine research in the transonic flow regime are available. These are the “Windtunnel for Straight Cascades” and the “Windtunnel for Rotating Cascades”. The Straight Cascade windtunnel is of blow-down type, operating in the Mach number range of 0.2 to 1.6. The Rotating Cascade Tunnel is a facility with closed flow path enabling the independent variation of Mach and Reynolds number. In the Rotating Cascade Tunnel the investigated objects range from isolated vanes to 1½ stages. In the following the features of the windtunnels will be described and some experimental results shown.
|Title:||Experimental Turbine Research at DLR Göttingen|
|Journal or Publication Title:||Journal of the Gas Turbine Society of Japan|
|In ISI Web of Science:||No|
|Page Range:||pp. 47-56|
|Keywords:||Turbomachinery, Turbine, Aerodynamics, Transonic Flow, Heat Transfer, Windtunnel, Cascade, Measurement Techniques|
|HGF - Research field:||Aeronautics, Space and Transport (old)|
|HGF - Program:||Aeronautics|
|HGF - Program Themes:||Propulsion Systems|
|DLR - Research area:||Aeronautics|
|DLR - Program:||L ER - Engine Research|
|DLR - Research theme (Project):||L - Turbine Technologies|
|Institutes and Institutions:||Institute of Propulsion Technology|
|Deposited By:||elib DLR-Beauftragter|
|Deposited On:||16 Sep 2005|
|Last Modified:||06 Jan 2010 13:33|
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