Basic flow cases were followed by flow control in which mainly air jet vortex generators were used. In: Proceedings of the 8th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, vol. 2, pp. 541–547 (2007)Google Scholar.

Basic flow cases were followed by flow control in which mainly air jet vortex generators were used. In addition, suction through the test wall was implemented, but only in the curved channel. This was done for comparison with earlier EUROSHOCK European project results. 6. Ryszard, . Piotr, . Krystyna, . Oskar, . Flow structure in the region of three shock wave interaction. Aerospace Science and Technology 8(6), 499–508 (2004)CrossRefGoogle Scholar.

Proceedings of the 9th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows (ISAIF9) 8~11 September 2009, Gyeongju, Korea. Experimental Facility. The measurements have been performed in the RC-1 facility of the von Karman Institute. The Time Resolved Particle Image Velocimetry (TR-PIV), described in provides accurate qualitative and quantitative information on the time evolution of the relative velocity and turbulence in a complete suction to pressure side plane of a rotating channel.

The 12th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows will be held from July 13 to July 16, 2015 in Lerici (SP), Italy, at Villa Marigola, a prestigious eighteenth century palace, center of conferences and exhibitions

The 12th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows will be held from July 13 to July 16, 2015 in Lerici (SP), Italy, at Villa Marigola, a prestigious eighteenth century palace, center of conferences and exhibitions. Lerici is a coastal city of north-western Italy, overlooking the famous Gulf of Poets, one of the most important seaside villages of Liguria and northern Italy in general. The Symposium includes 4 days of scientific and technological sessions.

Proceedings of 11th International Symposium on Experimental and Computational Aerothermodynamics of. .flow rate on the tested valve.

Proceedings of 11th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows May 6-11, 2013, Shenzhen, China. Numerical Simulations for Transonic Flow in Control Valve. system the pressure regulator was utilized on the outlet of. the second container. The regulator provided a real-time.

Proceedings of the 8th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows . consistent with that of experiments

Proceedings of the 8th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows . consistent with that of experiments. Nonetheless, the fact of good agreements between the calculation and experiment demonstrates the reliability of CFX results. The mass-flow rate of the forementioned computation and experiment is . kg/s. With the change of mass-flow rate, the inlet averaged velocity or characteristic Reynolds number will also vary

FCT, the International Symposia on Fundamentals of Computation Theory is a biennial series of conferences in the field of theoretical computer science.

FCT, the International Symposia on Fundamentals of Computation Theory is a biennial series of conferences in the field of theoretical computer science. FCT was previously held at the following institutions. Conferences in theoretical computer science.

4 Proceedings of the 8 th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows pressure distribution is typical. In supersonic part of the nozzle pressure is slightly lower than in the experiment due to lack of the sidewall boundary layer causing deceleration of the flow in the shock upstream supersonic part of the tunnel. Not surprisingly, the 3d computation matches almost exactly the measured data in this region