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4篇 您的检索式:作者名="P Doerffer"
    题名 作者 年代 出处 被引量
1Shock wave-boundary layer interaction control by wall ventilation 显示文摘Doerffer P Bohning R 2003Aerospace Science and Technolo- gy2003,,7:1
2Secondary Flow Control and Stream wise Vortices Formation 显示文摘Piotr P Doerffer Jochen Amecke 1994ASME Paper 94-GT-3761994,,:1
3An improved neural network for manufacturing cell formation显示文摘DOERFFER P SZULC O BOHNING R 2007Journal of Computer Science & Technology2007,21,6:1
4Numerical Simulation of the Tip Aerodynamics and Acoustics Test显示文摘The application of an efficient flow control system on helicopter rotor blades may lead to improved aerodynamic performance. Recently, our invention of Rod Vortex Generators(RVGs) has been analyzed for helicopter rotor blades in hover with success. As a step forward, the study has been extended to forward flight conditions. For this reason, a validation of the numerical modelling for a reference helicopter rotor(without flow control) is needed. The article presents a study of the flow-field of the AH-1G helicopter rotor in low-, medium- and high-speed forward flight. The CFD code FLOWer from DLR has proven to be a suitable tool for the aerodynamic analysis of the two-bladed rotor without any artificial wake modelling. It solves the URANS equations with LEA(Linear Explicit Algebraic stress) k-ω model using the chimera overlapping grids technique. Validation of the numerical model uses comparison with the detailed flight test data gathered by Cross J. L. and Watts M. E. during the Tip Aerodynamics and Acoustics Test(TAAT) conducted at NASA in 1981. Satisfactory agreements for all speed regimes and a presence of significant flow separation in high-speed forward flight suggest a possible benefit from the future implementation of RVGs. The numerical results based on the URANS approach are presented not only for a popular, low-speed case commonly used in rotorcraft community for CFD codes validation but preferably for medium- and high-speed test conditions that have not been published to date.F Tejero E P Doerffer O Szulc J L Cross 2016Journal of Thermal Science2016,25,2:0
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