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Georg May - Aerospace Computing Lab - Stanford University

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RESEARCH INTERESTS<br />

High order numerical methods for hyperbolic conservation laws on unstructured and<br />

structured meshes using pseudo-spectral and spectral methods.<br />

Kinetic schemes for computational fluid dynamics.<br />

Numerical algorithms for unstructured and general polyhedral meshes.<br />

Software development for scientific computing<br />

PROFESSIONAL EXPERIENCE<br />

Internship MTU Aero Engines, Munich, Germany (2001)<br />

Market analysis, civil aircraft. Performed statistical analysis and created reports for<br />

aircraft market prediction<br />

Engine predesign. Thermodynamic analysis of new aircraft engines<br />

Research assistant Shocktube laboratory, Aachen <strong>University</strong> (1998)<br />

Conducted experiments in rarefied gas dynamics<br />

PUBLICATIONS AND PRESENTATIONS<br />

LANGUAGES<br />

"A Spectral Difference Method for the Euler and Navier-Stokes Equations on Unstructured Meshes". AIAA-<br />

2006-0304 and 44th AIAA <strong>Aerospace</strong> Sciences Meeting and Exhibit, January 9-12, 2006, Reno,<br />

NV<br />

“High order accurate methods for high-speed flows”. AIAA Paper 2005-5251 and 17 th AIAA<br />

Computational Fluid Dynamics Conference, June 6-9, 2005, Toronto, Canada<br />

“Improved gas kinetic multigrid method for Three-Dimensional Computation of Viscous Flow”. AIAA Paper<br />

2005-5106 and 35 th AIAA Computational Fluid Dynamics Conference, June 6-9, 2005, Toronto,<br />

Canada<br />

“Calculation of three-dimensional transonic flow using a gas-kinetic BGK finite volume method”. AIAA Paper<br />

2005-1397 and 43 rd <strong>Aerospace</strong> Sciences Meeting and Exhibit, January 10-13, 2005, Reno, NV.<br />

“Unstructured algorithms for inviscid and viscous flows embedded in a unified solver architecture: Flo3xx”.<br />

AIAA Paper 2005-0318 and 43 rd <strong>Aerospace</strong> Sciences Meeting and Exhibit, January 10-13, 2005,<br />

Reno, NV<br />

“Drag Prediction for the DLR-F6 configuration”. AIAA Paper 2004-0396 and 42 nd <strong>Aerospace</strong> Sciences<br />

Meeting and Exhibit, January 5-8, 2004, Reno, NV<br />

Fluent in German and English<br />

Working knowledge in French and Latin<br />

TEACHING EXPERIENCE<br />

Teaching Assistant, Aachen <strong>University</strong>, Germany<br />

Graded problem sets for course in solid mechanics

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