Titlebook: MEGAFLOW - Numerical Flow Simulation for Aircraft Design; Results of the secon Norbert Kroll (Member of the Helmholtz Association Conferenc

Animosity

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書目名稱MEGAFLOW - Numerical Flow Simulation for Aircraft Design被引頻次學科排名




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書目名稱MEGAFLOW - Numerical Flow Simulation for Aircraft Design年度引用學科排名




書目名稱MEGAFLOW - Numerical Flow Simulation for Aircraft Design讀者反饋




書目名稱MEGAFLOW - Numerical Flow Simulation for Aircraft Design讀者反饋學科排名

壓倒

1612-2909 cs and fluid mechanics for aerospace and other applications.The aerospace industry increasingly relies on advanced numerical simulation tools in the early design phase. This volume provides the results of a German initiative which combines many of the CFD development activities from the German Aeros

electrolyte

Turbulence Models in FLOWer Results for industrially more relevant test cases of the flow around two different wing-body configurations and a three-element airfoil are presented, confirming the findings for the simple geometries at least under transonic conditions. From this, recommendations for the choice of suitable models are derived.

Lamina

Hybrid Grid Adaptation in TAUthe grid refinement with surface approximation and the . adjustment along wall-normal lines. Furthermore an overview of the used sensor functions is given, which are available for the detection of the local refinement and de-refinement.

效果

nullify

The Continuous Adjoint Approach in Aerodynamic Shape Optimizationmization methods based on the calculation of the derivatives of the cost function with respect to the design variables suffer from the high computational costs if many design variables are used. However, these gradients can be efficiently obtained by solution of the continuous adjoint flow equations.

自戀

Application of the Adjoint Technique with the Optimization Framework Synaps Pointer Proto multi-point optimization demonstrates the capability of the methodology to solve more complex problems. At the end, the body optimization and the wing optimization of a supersonic commercial aircraft confirm the flexibility of the framework and the efficiency of the adjoint technique.

fiction

1612-2909 pace Center (DLR), universities, and aircraft industry. Numerical algorithms for structured and hybrid Navier-Stokes solvers are presented in detail. The capabilities of the software for complex industrial applications are demonstrated..978-3-642-06365-7978-3-540-32382-2Series ISSN 1612-2909 Series E-ISSN 1860-0824

形容詞詞尾

bioavailability

Transition Modeling in FLOWer — Transition Prescription and Predictionthods were incorporated into the code and an infrastructure was built up in order to handle the underlying transition prediction strategy which results in an iteration process within the solution process of the RANS equations. Finally, physical models for the modeling of transitional flow were implemented and tested.