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Megadesign And Megaopt German Initiatives For Aerodynamic Simulation And Optimization In Aircraft Design Results Of The Closing Symposium Of The Megadesign And Megaopt Projects Braunschweig Germany 23 24 May 2007 1st Edition T Alrutz

  • SKU: BELL-4193438
Megadesign And Megaopt German Initiatives For Aerodynamic Simulation And Optimization In Aircraft Design Results Of The Closing Symposium Of The Megadesign And Megaopt Projects Braunschweig Germany 23 24 May 2007 1st Edition T Alrutz
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Megadesign And Megaopt German Initiatives For Aerodynamic Simulation And Optimization In Aircraft Design Results Of The Closing Symposium Of The Megadesign And Megaopt Projects Braunschweig Germany 23 24 May 2007 1st Edition T Alrutz instant download after payment.

Publisher: Springer-Verlag Berlin Heidelberg
File Extension: PDF
File size: 18.09 MB
Pages: 313
Author: T. Alrutz, D. Vollmer (auth.), Norbert Kroll, Dieter Schwamborn, Klaus Becker, Herbert Rieger, Frank Thiele (eds.)
ISBN: 9783642040924, 9783642040931, 3642040926, 3642040934
Language: English
Year: 2009
Edition: 1

Product desciption

Megadesign And Megaopt German Initiatives For Aerodynamic Simulation And Optimization In Aircraft Design Results Of The Closing Symposium Of The Megadesign And Megaopt Projects Braunschweig Germany 23 24 May 2007 1st Edition T Alrutz by T. Alrutz, D. Vollmer (auth.), Norbert Kroll, Dieter Schwamborn, Klaus Becker, Herbert Rieger, Frank Thiele (eds.) 9783642040924, 9783642040931, 3642040926, 3642040934 instant download after payment.

This volume contains results of the German CFD initiative MEGADESIGN which combines CFD development activities from DLR, universities and aircraft industry. Based on the DLR flow solvers FLOWer and TAU the main objectives of the four-years project is to ensure the prediction accuracy with a guaranteed error bandwidth for certain aircraft configurations at design conditions, to reduce the simulation turn-around time for large-scale applications significantly, to improve the reliability of the flow solvers for full aircraft configurations in the complete flight regime, to extend the flow solvers to allow for multidisciplinary simulations and to establish numerical shape optimization as a vital tool within the aircraft design process. This volume highlights recent improvements and enhancements of the flow solvers as well as new developments with respect to aerodynamic and multidisciplinary shape optimization. Improved numerical simulation capabilities are demonstrated by several industrial applications.

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