Multi-Point Design Optimization of Busemann Based Intakes for Scramjet-Powered Ascent Flight via Surrogate-Assisted Evolutionary Algorithms
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[1] Russell R. Boyce,et al. SCRAMSPACE : Scramjet-based access-to-space systems , 2011 .
[2] Russell R. Boyce,et al. Physical insight into scramjet inlet behaviour via multi-objective design optimisation , 2010 .
[3] I. Sobol. Uniformly distributed sequences with an additional uniform property , 1976 .
[4] H. Ogawa,et al. Multi-point design optimization of a high-performance intake for scramjet-powered ascent flight , 2020 .
[5] Raphael T. Haftka,et al. Surrogate-based Analysis and Optimization , 2005 .
[6] Ajay P. Kothari,et al. Streamline Tracing: Technique for Designing Hypersonic Vehicles , 2000 .
[8] E. T. Curran,et al. Scramjet Engines: The First Forty Years , 2001 .
[9] Charles McClinton,et al. X-43 - Scramjet Power Breaks the Hypersonic Barrier: Dryden Lectureship in Research for 2006 , 2006 .
[10] Tapabrata Ray,et al. A surrogate assisted parallel multiobjective evolutionary algorithm for robust engineering design , 2006 .
[11] Ryan P. Starkey. Scramjet Optimization for Maximum Off-Design Performance , 2004 .
[12] A. Forrester,et al. Exploring and Exploiting a Surrogate , 2008 .
[13] L. Richardson,et al. The Deferred Approach to the Limit. Part I. Single Lattice. Part II. Interpenetrating Lattices , 1927 .
[14] Russell R. Boyce,et al. The HyShot Scramjet Flight Experiment - Flight Data and CFD Calculations Compared , 2003 .
[15] W. Sutherland. LII. The viscosity of gases and molecular force , 1893 .
[16] F. Menter. Two-equation eddy-viscosity turbulence models for engineering applications , 1994 .
[17] Christophe Geuzaine,et al. Gmsh: A 3‐D finite element mesh generator with built‐in pre‐ and post‐processing facilities , 2009 .
[18] Russell R. Boyce,et al. Effects of leading-edge truncation and stunting on drag and efficiency of busemann intakes for axisymmetric scramjet engines , 2012 .
[19] Stephen Wornom,et al. Design and analysis of streamline traced hypersonic inlets , 1999 .
[20] Andreas K. Flock,et al. Viscous Effects and Truncation Effects in Axisymmetric Busemann Scramjet Intakes , 2016 .
[21] S. Moelder,et al. Busemann inlet for hypersonic speeds. , 1966 .
[22] M. Smart,et al. Effects of Oxygen Enrichment on Scramjet Performance , 2013 .
[23] Graham V. Candler,et al. Hypersonic inward turning inlets: Design and optimization , 2006 .
[24] G. Natarajan,et al. On Maximum Ballistic Coefficient Axisymmetric Geometries in Hypersonic Flows , 2017 .
[25] Michael K. Smart,et al. How much compression should a scramjet inlet Do , 2012 .
[26] M. Liou,et al. A New Flux Splitting Scheme , 1993 .