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A difference-fractional FOM decision method for down-selection of hypersonic compression system configurations

  • Published:2013-06 Issue:1 Volume:27 Page:147-155
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Sarosh Ali,Shi-Ming Chen,Yun-Feng Dong

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference23 articles.

1. Metamodels for Aerothermodynamic design optimization of spiked blunt bodies;Ahmed;Aerospace Science and Technology,2010

2. Optimal return to base cruise of hypersonic carrier vehicles;Bayer;Zeitschrift fur Flugwissenschaften and Weltraumforschung (ZFW),1992

3. Hypersonic Aerothermodynamics;Bertin,1994

4. Improvement of forebody/inlet integration for hypersonic vehicle;Bissinger;Aerospace Science and Technology,1998

5. Stage separation – aerodynamics and flow physics;Breitsamter,2005

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1. A Figure of Merit Based Computational Heat Transfer Method for Aerothermal Analysis of Airborne Electronics System LRU;2022 19th International Bhurban Conference on Applied Sciences and Technology (IBCAST);2022-08-16

2. Range Extension of Hypersonic Cruise Vehicle with Lowest Technical Merit;18th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference;2017-06-02

3. The GA-ANN expert system for mass-model classification of TSTO surrogates;Aerospace Science and Technology;2016-01

4. A Cognitive-Heuristic Framework for Optimization of Spaceplane-System Configurations;Advances in Intelligent Systems and Computing;2013-09-22
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