Titlebook: Computational Fluid Dynamics 2004; Proceedings of the T Clinton Groth,David W. Zingg Conference proceedings 20061st edition Springer-Verlag

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https://doi.org/10.1007/BFb0040067 low-Mach preconditioning matrix. The proposed approach exploits a particular property of a widely used low-Mach preconditioner proposed by Turkel. Its efficiency is demonstrated on some steady and unsteady applications.

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High-End Computing Challenges in Aerospace Design and Engineering. The paper discusses modeling capabilities needed for each challenge and presents projections of future near and far-term HEC computing requirements. NASA’s HEC Project Columbia is described and programming strategies presented that are necessary to achieve high real performance

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Numerical Simulation of the Oscillations in a Mixer - An Internal Aeroacoustic Feedback Systemk loop results in violent instabilities that are suspected of causing damage to some tunnel components. The computed frequency is in good agreement with the available experimental data. The physical phenomena are explained based on the numerical results.

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A Matrix-Free Implicit Method for Flows at All Speeds low-Mach preconditioning matrix. The proposed approach exploits a particular property of a widely used low-Mach preconditioner proposed by Turkel. Its efficiency is demonstrated on some steady and unsteady applications.

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