Optimization of hypersonic aircraft using genetic algorithms

Author:

Ahuja Vivek,Hartfield Roy J.,Shelton Andrew

Publisher

Elsevier BV

Subject

Applied Mathematics,Computational Mathematics

Reference15 articles.

1. C. Cockrell, W.C. Engelund, et al., Integrated aero-propulsive CFD methodology for the hyper-X flight experiment, in: AIAA 18TH Applied Aerodynamics Conference, AIAA Paper 2009-4010, 2000.

2. A. Frendi, On the CFD support for the hyper-X aerodynamic database, AIAA 99-0885.

3. M.J. Lewis, A hypersonic propulsion airframe integration overview, in: AIAA 2003-4405 presented at the AIAA/SAE/ASME/ASEE 39th Joint Propulsion Conference, Huntsville, AL, July 20–23, 2003.

4. Vivek Ahuja, Roy Hartfield, Optimization of scramjet combustor designs using genetic algorithms and CFD, in: AIAA 2008-5925 presented at the AIAA International Multidisciplinary Design and Optimization Conference (MDO), Victoria City, British Columbia, Canada, September 2008.

5. J.E. Bradford, A. Charania, J. Wallace, D.R. Eklund, Quicksat: a two-stage to orbit reusable launch vehicle utilizing air-breathing propulsion for responsive space access, in: AIAA 2004-5950, Space 2004 Conference and Exhibit, September 28–30, San Diego, CA, 2004.

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