The Continuous Adjoint Approach in Aerodynamic Shape Optimization-Reference-Cited by-同舟云学术

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The Continuous Adjoint Approach in Aerodynamic Shape Optimization

Published: Issue: Volume: Page:181-193
ISSN:
Container-title:MEGAFLOW - Numerical Flow Simulation for Aircraft Design
language:
Short-container-title:

Author:

Gauger N.R.,Brezillon J.

Publisher

Springer Berlin Heidelberg

Link

http://link.springer.com/content/pdf/10.1007/3-540-32382-1_13.pdf

Reference17 articles.

1. Kroll, N., Rossow, C.C., Becker, K. and Thiele, F., “The MEGAFLOW project”, Aerosp. Sci. Technol., Vol. 4, pp. 223–237, 2000.

2. Kroll, N., Rossow, C.C., Schwamborn, D., Becker, K. and Heller, G., “MEGAFLOW — A Numerical Flow Simulation Tool for Transport Aircraft Design”, ICAS 2002-1.10.5, 23rd International Congress of Aeronautical Sciences, Toronto, 2002.

3. Jameson, A., “Aerodynamic design via control theory”, Journal of Scientific Computing, Vol. 3, pp. 233–260,1988.

4. Jameson, A., “Computational aerodynamics for aircraft design”, Science, Vol. 245, pp. 361–371, 1989.

5. Jameson, A., “Optimum aerodynamic design via boundary control”, AGARDR-803, pp. 3.1–3.33, 1994.

Cited by 3 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Automatic transition from simulation to one-shot shape optimization with Navier-Stokes equations;GAMM-Mitteilungen;2010-10

2. An Efficient One-Shot Algorithm for Aerodynamic Shape Design;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2010

3. Single-step One-shot Aerodynamic Shape Optimization;International Series of Numerical Mathematics;2009

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