Maximum lift/drag hypersonic body shapes obtained with MINT as the
Download scientific diagram | Maximum lift/drag hypersonic body shapes obtained with MINT as the aerodynamic analysis code and: a) constrained DFP, and b) constrained GA. from publication: Invited lecture, EUROGEN'99 - Evolutionary Algorithms in Engineering and Computer Science: Recent Advances and Industrial Applications, Editors: K | Computer Science and Engineering | ResearchGate, the professional network for scientists.
George DULIKRAVICH, Ph.D.
PDF) Multidisciplinary Hybrid Constrained GA Optimization
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Spiked Blunt Bodies for Hypersonic Flights - GridPro Blog
Design: One of the major hurdles faced in attaining supersonic speeds by early fighters was the non-sweep design of the wings which increased drag considerably. Yet, the X1 Experimental aircraft had a
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Aerodisk effects on drag reduction for hypersonic blunt body with an ellipsoid nose - ScienceDirect
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PDF) Multidisciplinary Hybrid Constrained GA Optimization
Flowchart of automatic switching among modules in a hybrid
George DULIKRAVICH, Ph.D.