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Institutes and Facilities: Turbine Technologie

Number of items at this level: 8.

  Rehder, Hans-Jürgen (2008) Trailing Edge Film Cooling in a Transonic Cascade – Aerodynamic Experiments and Evaluation of Airfoil Loss Coefficients (European Research Project AITEB-2). DLR-Interner Bericht. IB 225-2008 A 03, 133 S. Volltext nicht online.

  Kondareddypally Nanjundappa, Abhishek and Rehder, Hans-Jürgen (2008) Design and Performance Investigations of a Transonic Turbine Rotor Cascade. DLR-Interner Bericht. 225-2008 A 01, 49 S. Volltext nicht online.

  Gieß, Peter-Anton and Mullaert, Arnold (2007) AN EXPERIMENTAL INVESTIGATION OF AN IMPROVED FILM-COOLING CONFIGURATION AT A TURBINE VANE ENDWALL TO REDUCE THE AMOUNT OF COOLANT. In: 7th European Conference on Turbomachinery, Fluid Dynamics and Thermodynamics, 5-9 March 2007, Athens-Greece, pp. 1095-1104. 7th European Conference on Turbomachinery, 2007-03-05 - 2007-03-09, Athens, Greece. Volltext nicht online.

  Elfert, Martin and Hoevel, Helmut (2006) Experimentelle Untersuchungen in rotierenden Kühlsystemen von Turbinenschaufeln. In: Tagungsband. 10. Statusseminar der AG TURBO, Verbundprojekt CO2-Reduktion durch Effizienz „COOREFF-T", 6. und 7. Dezember 2006, S. 7-1 - 7-11, DLR, Köln. Volltext nicht online.

  Rehder, Hans-Jürgen (2006) Experimentelle Untersuchungen des Strömungsfeldes von 2 Dampfturbinen-Leitradgittern der Fa. Siemens AG Anhang A. DLR-Interner Bericht. IB 225-2006 C01A, 98 S. Volltext nicht online.

  Elfert, Martin and Jarius, Marc (2005) Detailed Flow Investigation in a Ribbed Turbine Blade Two-Pass Cooling System. In: 17th Int. Symp. on Air Breathing Engines (XVII ISABE), Sept. 4-9, 2005, Munich, Germany (ISABE-2005-1115), pp. 1-10. ISABE Conference, Sept. 4-9, 2005, Munich (Germany). ISBN 1-56347-790-4. Volltext nicht frei.

  Rehder, H.-J. (2005) Throughflow Analysis and NGV Effects Assessment for the DLR Rig. DLR-Interner Bericht. 225-2005 A 05, 49 S. Volltext nicht online.

  Ochrymiuk, T. and Gieß, P.-A. and Kost, F. (2004) Experimental Investigations of the Flow Field within a Gas Turbine Rotor Cascade without Coolant Ejection Designed by RRD. Appendix A. DLR-Interner Bericht. 225-2003 C 07A, 166 S. Volltext nicht online.

This list was generated on Sun Jun 16 03:44:13 2013 CEST.
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