Titlebook: New Results in Numerical and Experimental Fluid Mechanics VI; Contributions to the Cameron Tropea,Suad Jakirlic,Heinz H?nlinger Conference

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書(shū)目名稱(chēng)New Results in Numerical and Experimental Fluid Mechanics VI影響因子(影響力)學(xué)科排名




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書(shū)目名稱(chēng)New Results in Numerical and Experimental Fluid Mechanics VI網(wǎng)絡(luò)公開(kāi)度學(xué)科排名




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溫和女人

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Multiple Discipline Take-Off Weight Minimization for a Supersonic Transport Aircraftst flight time is spent-the disciplines aerodynamics and structures are modelled at high fidelity while other contributing disciplines and flight phases are modelled less accurate. For a generic long-range mission the impact of the supersonic cruise-speed on the minimal take-off weight (enabling to cruise this long range mission) is addressed.

狗舍

High-Reynolds-Number Design of a Wing Section Including Control of Boundary Layer Propertieshe boundary layer properties. Three airfoils were created for transonic free flight conditions with very similar aerodynamic performance, but different boundary layer developments on the upper surface. The performance and boundary layer properties of the airfoils were discussed and validated by RANS computations.

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出生

Shock Control Bumps on Flexible and Trimmed Transport Aircraft in Transonic Flow plane was investigated. Flexibility of the wing-body model was considered and the influence of aeroelasticity on the SCB performance was examined. RANS simulations with the DLR FLOWer code showed, that both the influence of trimming as well as of aeroelasticity is negligible for SCB design.

騷擾

驚呼

Pressure and Heat Flux Measurements on the Surface of a Low-Aspect-Ratio Circular Cylinder Mounted oresolution was used to investigate the heat flux fluctuation on the surface of a slightly heated cylinder. Comparative investigations showed qualitative correlations between the pressure and heat flux fluctuations around the cylinder and on its free-end. Several flow features could be identified by means of time-resolved surface measurements.

褻瀆

議程

Three-Dimensional Discontinuous Galerkin Codes to Simulate Viscous Flow by Spatial Discretization ofn extension will be provided to include both three-dimensional flows and curved elements to properly represent three-dimensional bodies with curvature. Some results, like Sows around a sphere and around an Onera M6 wing, are calculated and compared with experiments.