Multipoint Design Optimization of Busemann-Based Intakes for Scramjet-Powered Ascent Flight

Scramjet engines are one of the most promising hypersonic airbreathing propulsion technologies for robust, efficient, and economical access to space. Multi-objective design optimization has been co...

[1]  Christophe Geuzaine,et al.  Gmsh: A 3‐D finite element mesh generator with built‐in pre‐ and post‐processing facilities , 2009 .

[2]  Michael K. Smart,et al.  Flight Data Analysis of the HyShot 2 Scramjet Flight Experiment , 2006 .

[3]  Russell R. Boyce,et al.  Effects of leading-edge truncation and stunting on drag and efficiency of busemann intakes for axisymmetric scramjet engines , 2012 .

[4]  M. Liou,et al.  A New Flux Splitting Scheme , 1993 .

[5]  Charles R. Mcclinton,et al.  Preliminary X-43 flight test results , 2005 .

[6]  Russell R. Boyce,et al.  Physical insight into scramjet inlet behaviour via multi-objective design optimisation , 2010 .

[7]  Andreas K. Flock,et al.  Viscous Effects and Truncation Effects in Axisymmetric Busemann Scramjet Intakes , 2016 .

[8]  S. Moelder,et al.  Busemann inlet for hypersonic speeds. , 1966 .

[9]  William H. Heiser,et al.  Hypersonic Airbreathing Propulsion , 1994 .

[11]  Akira Nagashima,et al.  Viscosity and thermal conductivity of dry air in the gaseous phase , 1985 .

[12]  Ajay P. Kothari,et al.  Streamline Tracing: Technique for Designing Hypersonic Vehicles , 2000 .

[13]  J. Anderson,et al.  Modern Compressible Flow: With Historical Perspective , 1982 .

[14]  F. Menter.  Two-equation eddy-viscosity turbulence models for engineering applications , 1994 .

[15]  A. Forrester,et al.  Exploring and Exploiting a Surrogate , 2008 .

[16]  Russell R. Boyce,et al.  Shock tunnel and numerical studies of a large inlet-fuelled inward turning axisymmetric scramjet , 2012 .

[17]  L. Richardson,et al.  The Deferred Approach to the Limit. Part I. Single Lattice. Part II. Interpenetrating Lattices , 1927 .

[18]  Kalyanmoy Deb,et al.  A fast and elitist multiobjective genetic algorithm: NSGA-II , 2002, IEEE Trans. Evol. Comput..

[19]  G. Natarajan,et al.  On Maximum Ballistic Coefficient Axisymmetric Geometries in Hypersonic Flows , 2017 .

[20]  W. Sutherland.  LII. The viscosity of gases and molecular force , 1893 .

[21]  M. Smart,et al.  Effects of Oxygen Enrichment on Scramjet Performance , 2013 .

[22]  Tapabrata Ray,et al.  A surrogate assisted parallel multiobjective evolutionary algorithm for robust engineering design , 2006 .

[23]  I. Sobol.  Uniformly distributed sequences with an additional uniform property , 1976 .

[24]  H. Ogawa,et al.  Multi-point design optimization of a high-performance intake for scramjet-powered ascent flight , 2020 .

[25]  Ryan P. Starkey.  Scramjet Optimization for Maximum Off-Design Performance , 2004 .

[26]  Javier Urzay,et al.  Supersonic Combustion in Air-Breathing Propulsion Systems for Hypersonic Flight , 2018 .

[27]  E. T. Curran,et al.  Scramjet Engines: The First Forty Years , 2001 .

[28]  Raphael T. Haftka,et al.  Surrogate-based Analysis and Optimization , 2005 .