Comment on “Parametric Ideal Scramjet Cycle Analysis”

Abstract

No AccessTechnical CommentComment on “Parametric Ideal Scramjet Cycle Analysis”Qingchun Yang, Juntao Chang, Duo Zhang, Jichao Hu and Wen BaoQingchun YangSchool of Energy Science and Engineering, Harbin Institute of Technology, 150001 Heilongjiang, People’s Republic of China*School of Energy Science and Engineering; .Search for more papers by this author, Juntao ChangSchool of Energy Science and Engineering, Harbin Institute of Technology, 150001 Heilongjiang, People’s Republic of China†Associate Professor, School of Energy Science and Engineering; .Search for more papers by this author, Duo ZhangSchool of Energy Science and Engineering, Harbin Institute of Technology, 150001 Heilongjiang, People’s Republic of China‡School of Energy Science and Engineering; .Search for more papers by this author, Jichao HuSchool of Energy Science and Engineering, Harbin Institute of Technology, 150001 Heilongjiang, People’s Republic of China§School of Energy Science and Engineering; .Search for more papers by this author and Wen BaoSchool of Energy Science and Engineering, Harbin Institute of Technology, 150001 Heilongjiang, People’s Republic of China¶Professor, School of Energy Science and Engineering; . Member AIAA.Search for more papers by this authorPublished Online:5 Feb 2015https://doi.org/10.2514/1.T4379SectionsView Full TextPDFPDF Plus ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Roux J. A., “Parametric Ideal Scramjet Cycle Analysis,” Journal of Thermophysics and Heat Transfer, Vol. 25, No. 4, 2011, pp. 581–585. doi:https://doi.org/10.2514/1.T3758 JTHTEO 0887-8722 LinkGoogle Scholar[2] Cui T., Yang S. and Yu D., “Ideal Heat Release of Supersonic Combustion,” Journal of Propulsion and Power, Vol. 29, No. 3, 2013, pp. 621–627. doi:https://doi.org/10.2514/1.B34735 JPPOEL 0748-4658 LinkGoogle Scholar[3] Roux J. A., Shakya N. and Choi J., “Revised Parametric Ideal Scramjet Cycle Analysis,” Journal of Thermophysics and Heat Transfer, Vol. 27, No. 1, 2013, pp. 178–183. doi:https://doi.org/10.2514/1.T3961 JTHTEO 0887-8722 LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byMode transition analysis of a turbine-based combined-cycle considering ammonia injection pre-compressor cooling and variable-geometry ram-combustorEnergy, Vol. 261Effect of Distributed Fuel Injection on Model Scramjet Combustor PerformanceMithuun Kanapathipillai, Minwook Chang, Andrew Yu, Camilo Aguilera and Kenneth Yu17 August 2020Thermodynamic efficiency analysis and cycle optimization of deeply precooled combined cycle engine in the air-breathing modeActa Astronautica, Vol. 138Constant Velocity Combustion Parametric Ideal Scramjet Cycle AnalysisJ. A. Roux and L. S. Tiruveedula22 February 2016 | Journal of Thermophysics and Heat Transfer, Vol. 30, No. 3Constant static-temperature heating for hydrogen fueled scramjet engineInternational Journal of Hydrogen Energy, Vol. 41, No. 3 What's Popular Volume 29, Number 1January 2015 CrossmarkInformationCopyright © 2014 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. Copies of this paper may be made for personal or internal use, on condition that the copier pay the $10.00 per-copy fee to the Copyright Clearance Center, Inc., 222 Rosewood Drive, Danvers, MA 01923; include the code 1533-6808/14 and $10.00 in correspondence with the CCC. TopicsAerodynamicsAeronautical EngineeringAeronauticsAirbreathing Jet EngineAircraft EnginesCombustion ChambersCombustorsEquations of Fluid DynamicsFluid DynamicsFluid MechanicsJet EnginesNozzlesPropulsion and PowerRamjetRocket EngineRocketryScramjet KeywordsScramjet EnginesFreestream VelocityCombustorsStatic PressureTurbojetRamjetCombustion ProcessExhaust NozzlesBrayton CyclePropulsive Efficiency Received15 January 2014Accepted16 July 2014Published online5 February 2015