Dissertations / Theses on the topic 'Scramjet'
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Matthews, Alexander J. "Scramjet intakes." Thesis, University of Oxford, 2003. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.400217.
Full textOdam, Judy. "Scramjet experiments using radical farming /." [St. Lucia, Qld.], 2004. http://adt.library.uq.edu.au/public/adt-QU20041206.101729/index.html.
Full textSchütte, Gerrit. "Probabilistische Untersuchungen zu Scramjet-Antriebssystemen." Aachen Shaker, 2009. http://d-nb.info/1000474291/04.
Full textMcGuire, Jeffrey Robert Aerospace Civil & Mechanical Engineering Australian Defence Force Academy UNSW. "Ignition enhancement for scramjet combustion." Awarded by:University of New South Wales - Australian Defence Force Academy. School of Aerospace, Civil and Mechanical Engineering, 2007. http://handle.unsw.edu.au/1959.4/38748.
Full textBiasca, Rodger Joseph. "Chemical kinetics of SCRAMJET propulsion." Thesis, Massachusetts Institute of Technology, 1988. http://hdl.handle.net/1721.1/35949.
Full textGardner, Anthony D. "HyShot scramjet testing in the HEG /." Köln : DLR, Bibliotheks- und Informationswesen, 2007. http://bvbr.bib-bvb.de:8991/F?func=service&doc_library=BVB01&doc_number=016271138&line_number=0001&func_code=DB_RECORDS&service_type=MEDIA.
Full textMaddalena, Luca. "Investigations of Injectors for Scramjet Engines." Diss., Virginia Tech, 2007. http://hdl.handle.net/10919/28683.
Full textPh. D.
Ingenito, Antonella. "Modellistica della combustione in regime supersonico." Doctoral thesis, La Sapienza, 2006. http://hdl.handle.net/11573/917117.
Full textPrebola, John L. Jr. "Performance of a Plasma Torch with Hydrocarbon Feedstocks for Use in Scramjet Combustion." Thesis, Virginia Tech, 1998. http://hdl.handle.net/10919/36941.
Full textMaster of Science
Rowan, Scott A. "Viscous drag reduction in a scramjet combustor /." St. Lucia, Qld, 2003. http://www.library.uq.edu.au/pdfserve.php?image=thesisabs/absthe17438.pdf.
Full textBrandstetter, Armin Johann Leopold. "Betriebsverhalten einer Dualmodus-SCRamjet-Modellbrennkammer mit Wasserstoffverbrennung." [S.l. : s.n.], 2004. http://deposit.ddb.de/cgi-bin/dokserv?idn=974166103.
Full textKarl, Sebastian. "Numerical Investigation of a Generic Scramjet Configuration." Doctoral thesis, Saechsische Landesbibliothek- Staats- und Universitaetsbibliothek Dresden, 2011. http://nbn-resolving.de/urn:nbn:de:bsz:14-qucosa-68695.
Full textStaustrahlantriebe, bei denen sich die Strömung im gesamten Triebwerksbereich im Überschall befindet (supersonic combustion ramjets, Scramjets), stellen ein - zumindest theoretisch - effektives Antriebessystem für den Hyperschallflug im Machzahlbereich von M > 5 dar. Die Auslegung und der Entwurf von luftatmenden Hyperschallantrieben sind in der Praxis mit Schwierigkeiten verbunden. Der Einsatz von Bodenversuchsanlagen ist auf kleinskalige Konfigurationen oder einzelne Triebwerkskomponenten begrenzt. Die Ergebnisse von numerischen Strömungssimulationsverfahren sind mit hohen Unsicherheiten behaftet, die ihren Ursprung in der Modellbildung für die komplexen Strömungsphänomene in chemisch reagierenden, kompressiblen und turbulenten Über- und Hyperschallströmungen haben. Weiterhin existieren keine allgemein gültigen Skalierungsgesetze um Aussagen aus Windkanalexperimenten auf Flugkonfigurationen zu übertragen.Die vorliegende Arbeit beschäftigt sich in diesem Zusammenhang mit der Erweiterung des DLRStrömungslösers TAU für die Berechnung von Überschallverbrennungsphänomenen in Scramjets sowie mit der Anwendung des Verfahrens für die numerische Analyse von Windkanalexperimenten, die im Hochenthalpiekanal Göttingen (HEG) des Deutschen Zentrums für Luft- und Raumfahrt (DLR) zur Untersuchung der generischen HyShot II Scramjet-Konfiguration durchgeführt wurden. Die wichtigsten Ziele waren die genaue Charakterisierung der freien Anströmung im Windkanal, der Nachweis der Anwendbarkeit des verwendeten Rechenverfahrens und die Analyse des Einflusses verschiedener numerischer Modellierungsansätze für die Strömungssimulation in Scramjets sowie die Nutzung der numerischen Daten für eine verbesserte Interpretation der experimentellen Ergebnisse
Munro, Stuart. "Scramjet Intakes: Designing for Performance and Operability." Thesis, University of Oxford, 2007. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.491519.
Full textSchütte, Gerrit [Verfasser]. "Probabilistische Untersuchungen zu Scramjet-Antriebssystemen / Gerrit Schütte." Aachen : Shaker, 2010. http://d-nb.info/1124364838/34.
Full textHoste, Jimmy-John O. E. "Scramjet combustion modeling using eddy dissipation model." Thesis, University of Strathclyde, 2018. http://digitool.lib.strath.ac.uk:80/R/?func=dbin-jump-full&object_id=30307.
Full textHalter, Megaera C. "Energy-turns analysis for a scramjet powered missle." Thesis, Virginia Tech, 1988. http://hdl.handle.net/10919/43753.
Full textA reduced order model describing the energy and heading angle
dynamics of a scramjet missile is developed using a singular
perturbation technique. The cruise analysis is briefly reviewed to
determine the conditions at which the missile will cruise most
efficiently. The turn and climb performance of the missile over the
conditions of interest is then examined and a family of extremal
trajectories is constructed which asymptotically approach the cruise at
an intermediate altitude.
Master of Science
Barone, Dominic L. "Investigation of TDLAS Measurements in a Scramjet Engine." University of Cincinnati / OhioLINK, 2010. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1277130335.
Full textOmari, Dennis. "Control of Transient Unstart in Isolator of Scramjet." The Ohio State University, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=osu1523367091946973.
Full textFrost, Myles Alexander. "Hyshot scramjet experiments in the T4 shock tunnel /." [St. Lucia, Qld.], 2001. http://www.library.uq.edu.au/pdfserve.php?image=thesisabs/absthe16919.pdf.
Full textFuhrmann, Thomas. "Auslegung und Betriebsverhalten von SCRamjet-Antriebssystemen für Raumtransporter-Hyperschallflugzeuge." München Verl. Dr. Hut, 2009. http://mediatum2.ub.tum.de/node?id=735781.
Full textTran, Kathleen. "One Dimensional Analysis Program for Scramjet and Ramjet Flowpaths." Thesis, Virginia Tech, 2010. http://hdl.handle.net/10919/30857.
Full textMaster of Science
Fuhrmann, Sirka [Verfasser]. "Gestufte Injektion und Verbrennung in einer Scramjet-Brennkammer / Sirka Fuhrmann." München : Verlag Dr. Hut, 2013. http://d-nb.info/1033041815/34.
Full textFrauholz, Sarah [Verfasser]. "Advanced Numerical Investigations of Hypersonic Scramjet Intake Flows / Sarah Frauholz." München : Verlag Dr. Hut, 2015. http://d-nb.info/107406318X/34.
Full textRock, Christopher. "Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors." Diss., Virginia Tech, 2010. http://hdl.handle.net/10919/77208.
Full textPh. D.
Zinnecker, Alicia M. "Modeling for Control Design of an Axisymmetric Scramjet Engine Isolator." The Ohio State University, 2012. http://rave.ohiolink.edu/etdc/view?acc_num=osu1354215841.
Full textMURUGAPPAN, SHANMUGAM. "INNOVATIVE TECHNIQUES TO IMPROVE MIXING AND PENETRATION IN SCRAMJET COMBUSTORS." University of Cincinnati / OhioLINK, 2005. http://rave.ohiolink.edu/etdc/view?acc_num=ucin1109697512.
Full textLarios-Barbosa, Jaime Omar. "SHOCK CORRELATION INVESTIGATION IN A GASEOUS FUELED AXISYMMETRIC SCRAMJET FLOWPATH." Wright State University / OhioLINK, 2013. http://rave.ohiolink.edu/etdc/view?acc_num=wright1377130377.
Full textMiki, Kenji. "Simulation of magnetohydrodynamics turbulence with application to plasma-assisted supersonic combustion." Diss., Atlanta, Ga. : Georgia Institute of Technology, 2009. http://hdl.handle.net/1853/26605.
Full textCommittee Chair: Menon Suresh; Committee Co-Chair: Jagoda Jeff; Committee Member: Ruffin Stephen; Committee Member: Thorsten Stoesser; Committee Member: Walker Mitchell. Part of the SMARTech Electronic Thesis and Dissertation Collection.
Brewer, Keith Merritt. "Exergy Methods for the Mission-Level Analysis and Optimization of Generic Hypersonic Vehicles." Thesis, Virginia Tech, 2006. http://hdl.handle.net/10919/32007.
Full textMaster of Science
Markell, Kyle Charles. "Exergy Methods for the Generic Analysis and Optimization of Hypersonic Vehicle Concepts." Thesis, Virginia Tech, 2005. http://hdl.handle.net/10919/31256.
Full textMaster of Science
Stewart, Benjamin S. "Predicted scramjet testing capabilities of the proposed RHYFL-X expansion tube /." [St. Lucia, Qld], 2004. http://www.library.uq.edu.au/pdfserve.php?image=thesisabs/absthe18241.pdf.
Full textFischer, Christian Max [Verfasser]. "Investigation of the isolator flow of scramjet engines / Christian Max Fischer." Aachen : Hochschulbibliothek der Rheinisch-Westfälischen Technischen Hochschule Aachen, 2014. http://d-nb.info/1059796627/34.
Full textKrause, Martin [Verfasser]. "Numerical Analysis of Transition Effects for SCRamjet Intake Flows / Martin Krause." Aachen : Shaker, 2010. http://d-nb.info/1101185546/34.
Full textCocks, Peter. "Large eddy simulation of supersonic combustion with application to scramjet engines." Thesis, University of Cambridge, 2011. https://www.repository.cam.ac.uk/handle/1810/239344.
Full textMundis, Nathan L. "Magnetohydrodynamic power generation in a scramjet using a post combustor generator." Diss., Rolla, Mo. : University of Missouri-Rolla, 2007. http://scholarsmine.umr.edu/thesis/pdf/Mundis_09007dcc8043ee98.pdf.
Full textVita. The entire thesis text is included in file. Title from title screen of thesis/dissertation PDF file (viewed March 25, 2008) Includes bibliographical references (p. 95-97).
Nguyen, Tran Quang Tue [Verfasser]. "Numerical investigations of relaminarization in scramjet flows / Tran Quang Tue Nguyen." Aachen : Hochschulbibliothek der Rheinisch-Westfälischen Technischen Hochschule Aachen, 2012. http://d-nb.info/1023093197/34.
Full textCorbin, Christopher Ryan. "Design and Analysis of a Mach 3 Dual Mode Scramjet Combustor." Wright State University / OhioLINK, 2008. http://rave.ohiolink.edu/etdc/view?acc_num=wright1208370076.
Full textMilligan, Ryan Timothy. "DUAL MODE SCRAMJET: A COMPUTATIONAL INVESTIGATION ON COMBUSTOR DESIGN AND OPERATION." Wright State University / OhioLINK, 2009. http://rave.ohiolink.edu/etdc/view?acc_num=wright1251725076.
Full textBurger, Scott Kuhlman. "Investigation of Injectant Molecular Weight and Shock Impingement Effects on Transverse Injection Mixing in Supersonic Flow." Thesis, Virginia Tech, 2010. http://hdl.handle.net/10919/31981.
Full textMaster of Science
Cox-Stouffer, Susan K. Jr. "Numerical Simulation of Injection and Mixing in Supersonic Flow." Diss., Virginia Tech, 1997. http://hdl.handle.net/10919/29628.
Full textPh. D.
Robinson, Matthew J. "Simultaneous lift, moment and thrust measurement on a scramjet in hypervelocity flow /." [St. Lucia, Qld.], 2003. http://www.library.uq.edu.au/pdfserve.php?image=thesisabs/absthe17611.pdf.
Full textHäberle, Jürgen. "Untersuchungen zum externen und internen Strömungsfeld eines Scramjet-Triebwerkseinlaufs bei unterschiedlichen Betriebspunkten." Köln DLR, Bibliotheks- und Informationswesen, 2009. http://d-nb.info/997418524/34.
Full textGriffiths, Alan David, and alan griffiths@anu edu au. "Development and demonstration of a diode laser sensor for a scramjet combustor." The Australian National University. Faculty of Science, 2005. http://thesis.anu.edu.au./public/adt-ANU20051114.132736.
Full textMattson, Erik Anthony. "An implicit algorithm for analysis of an airframe-integrated scramjet propulsion cycle." Thesis, Massachusetts Institute of Technology, 1988. http://hdl.handle.net/1721.1/35947.
Full textMcGillivray, Nathan T. "Coupling Computational Fluid Dynamics Analysis and Optimization Techniques for Scramjet Engine Design." Wright State University / OhioLINK, 2018. http://rave.ohiolink.edu/etdc/view?acc_num=wright1536311445147862.
Full textEugênio, Ribeiro Fábio Henrique. "Numerical Simulation of Turbulent Combustion in Situations Relevant to Scramjet Engine Propulsion." Thesis, Chasseneuil-du-Poitou, Ecole nationale supérieure de mécanique et d'aérotechnique, 2019. http://www.theses.fr/2019ESMA0001/document.
Full textScramjet engines are high-speed air breathing propulsion systems that do not require rotating elements to compress the air inlet stream. The flow is compressed dynamically through a supersonic intake system integrated in the aircraft’s forebody, reaching the required pressure and temperature for combustion to proceed within the combustor in this kind of engine. The combustion chamber is crossed by a supersonic flow, which limits severely the time available to inject fuel, mix it with oxidizer, ignite the resulting mixture and reach complete combustion. Cavities can be used to increase the residence time without excessive total pressure loss and are therefore used as flame holders in supersonic combustors.This thesis focuses in studying the flame stabilization mechanism and turbulence-chemistry interactions for a jet in a supersonic crossflow (JISCF) of vitiated air with hydrogen injection upstream of a wall-mounted squared cavity. The corresponding reactive high-speed flow conditions are scrutinized on the basis of numerical simulations of a scramjet model representative of experiments previously conducted at the University of Michigan. The computations are performed with the high-performance computational solver CREAMS, developed to perform the numerical simulation of compressible reactive multi-component flows on massively-parallel architectures. The solver makes use of high-order precision numerical schemes applied on structured meshes and the combustion chamber geometry is modeled by using the Immersed Boundary Method (IBM) algorithm. The present set of computations is conducted within the LES framework and the subgrid viscosity is treated with the wall-adapting local eddy (WALE)model. Two distinct temperatures are considered in the inlet vitiated airstream to study combustion stabilization. Special emphasis is placed on the analysis of the reactive flow topology and structure,and the combustion regimes are analyzed on the basis of standard turbulent combustion diagrams
Griffiths, Alan David. "Development and demonstration of a diode laser sensor for a scramjet combustor /." View thesis entry in Australian Digital Theses, 2005. http://thesis.anu.edu.au/public/adt-ANU20051114.132736/index.html.
Full textMalo-Molina, Faure Joel. "Numerical study of innovative scramjet inlets coupled to combustors using hydrocarbon-air mixture." Diss., Georgia Institute of Technology, 2010. http://hdl.handle.net/1853/33906.
Full textAngus, William J. "An investigation into the performance characteristics of a solid fuel scramjet propulsion device." Thesis, Monterey, California. Naval Postgraduate School, 1991. http://hdl.handle.net/10945/28306.
Full textRen, Chiang-Hwa. "A computer based model for the performance analysis of a SCRAMJET propulsion system." Thesis, Massachusetts Institute of Technology, 1989. http://hdl.handle.net/1721.1/39017.
Full text