Scramjet missile design using genetic algorithms-Reference-Cited by-同舟云学术

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Scramjet missile design using genetic algorithms

Published:2006-03 Issue:2 Volume:174 Page:1539-1563
ISSN:0096-3003
Container-title:Applied Mathematics and Computation
language:en
Short-container-title:Applied Mathematics and Computation

Author:

Hartfield R.J.,Burkhalter J.E.,Jenkins R.M.

Publisher

Elsevier BV

Subject

Applied Mathematics,Computational Mathematics

Reference9 articles.

1. Elements of Gas Turbine Propulsion;Mattingly,1996

2. The Aerodynamic Design of Aircraft;Kuchemann,1978

3. Hypersonic and High Temperature Gas Dynamics;Anderson,1989

4. Modern compressible flow with historical perspective;Anderson,1990

5. Nonequilibrium Hypersonic Aerothermodynamics;Park,1990

Cited by 9 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. Conceptual design and optimization of scramjet engines using the exergy method;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2018-11-07

2. Efficient Framework for Missile Design and 6DoF Simulation using Multi-fidelity Analysis and Data Fusion;17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2016-06-10

3. Adaptive Multifidelity Constraints Method for Efficient Multidisciplinary Missile Design Framework;Journal of Spacecraft and Rockets;2016-01

4. Optimization of Scramjet Combustor Geometries Using Genetic Algorithms;Journal of Propulsion and Power;2015-09

5. Optimization of hypersonic aircraft using genetic algorithms;Applied Mathematics and Computation;2014-09

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