By Manfred Griehl

All of the books that include the Luftwaffe Profile sequence encompasses a number of unique close-up pictures, occasionally in color, line drawings and an accompanying textual content that describes the planes and the theatres within which they operated.

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Fr/CONGRES/ERCOFTAC/database/. 46 Two other major CFD validation activities in the 90's provided blind test cases for turbomachinery internal flows: • The ASME test case of the NASA transonic compressor rotor 37, Strazisar and Denton (1995) • The lAHR/ERCOFTAC studies of a draft tube for a Francis Turbine, Gebart et al. (2000)). The participants in these vaUdation exercises were provided with sufficient information on the geometry and boundary conditions to set up and run a simulation, but the full test results were not made available.

Much of the progress achieved in this period is documented in the first major attempt to produce a complete set of test cases for turbomachinery flow validation - the AGARD Advisory Report on test cases for the computation of internal flows in aero engine components (Fottner (1990)). This work not only includes some usefiil test cases for steadyflowproblems in axial turbomachinery, but also the participants felt the need to make some usefiil general remarks on the set up and requirements of such test cases for the evaluation offlowprediction methods (Chapter II) and on the validity and accuracy of experimental data (Chapter III).

229-253. El Tahry S. H. C. 1992, Directions in Turbulence Modeling for in-Cylinder Flows in Reciprocating IC Engines, AIAA J. Prop power. 8,1040-1048. 54 36 [17] Huilai Zhang, Toshio Kobayashi, and Nobuyuki Taniguchi, 2000, Large Eddy Simulation of Motored Engine, Fisita, Seoul. C. and Jansen K. 1996, "LES on unstructured deforming meshes: Towards reciprocating IC engines". Center of Turbulence Research, Proceedings of the Summer Program. 54. [20] Reitz R. D. 21, pp. 173-196, Prog. Energy Combustion sci..

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