Univ.- Prof. Dr.-Ing. Christian Mundt
Univ.-Prof. Dr. Ing. Christian Mundt
Professur für Aerothermodynamik
Gebäude 35/Raum 2152
Telefon: +49 (0)89 6004 2076
eMail: christian.mundt@unibw.de
Veröffentlichungen
S.Saegeler, J. Lieser, Ch. Mundt: Improved modelling of vortical mixing for the simulation of efficient propulsion systems, acc. for 28th ICAS Congress, Brisbane, 2012.
A.Sventitskiy, Ch. Mundt: Application of the Narrow-band Correlated k-Distribution Method to Numerical Simulation of the IR Emission from Non-Scattering Exhaust Plumes, acc. for 43 AIAA Thermophysics Conf., 2012.
F.Göbel, J. Vos, Ch. Mundt; CFD Simulation of the FIRE II Flight Experiment, acc. for 42nd AIAA Fluid Dynamics Conference and Exhibit, 2012.
A.Sventitskiy, Ch. Mundt: Simulation of the IR Emission from non-scattering aircraft engine exhaust plumes using statistical narrowband model. acc. for 43 AIAA Thermophysics Conf., 2012.
S. Saegeler, Ch. Mundt: Verbesserte Simulation der Mischung in Triebwerksstrahlen, STAB Tagung, DLR Göttingen, 2011.
M. Kirschner, Ch. Mundt: Particle Image Velocimetrie in einem Hochenthalpiefreistrahl, STAB Tagung, DLR Göttingen, 2011.
Ch. Mundt, A. Sventitskiy, J. Cehelsky, A. Patters, M. Tservistas, M. Hahn, G. Juhl., J. deVincenzo: Assessing the safety of a mask designed for efficient delivery of aerosols to infants, submitted to Journ. Aerosol Medicine and Pulmonary Drug Delivery, 2011.
V. Lorenz, Ch. Mundt: On the numerical solution method of the 2D Oswatitsch Equations for Hypersonic Flow, 18th Int. Symp. Shock Waves, Manchester, 2011.
H. Griebel, R. Förstner, Ch. Mundt, A. Mohr, W. Mai, J. Polkko, H. Teodorescu, G. Herderich, S. Fasoulas, T. Marynowski, A. Stamminger, D. Heyner: The mission MIRIAM-2: Putting a gossamer ballute through an atmospheric entry flight test, Int. Planet. Probe Workshop, 2011.
F. Göbel, Ch. Mundt: CFD Analysis of Radiative Heat Transfer in the SSME Main Combustion Chamber using Advanced Spectral Models, 7th Eur. Symp. on Aerothermodynamics for Space Vehicles, 2011.
M. Starkloff, Ch. Mundt: Accurate interpolation of state surfaces for the thermodynamic properties of equilibrium carbon dioxide – nitrogen atmospheres and their implementation in a coupled Euler – boundary layer method, 3rd Int. ARA conference AA 1-2011-37, 2011.
D. Kliche, Ch. Mundt: Progress in multidisciplinary analysis and evaluation of supersonic combustion ramjets, AIAA-2011-2281, 17. AIAA Int. Space Planes and Hypersonic Systems and Technologies Conf., 2011.
P. Altenhöfer, T. Sander, Ch. Mundt: Measurements of temperature in shock tunnels using Laser-induced Transient gratings, AIAA-2011-2211, 17. AIAA Int. Space Planes and Hypersonic Systems and Technologies Conf., 2011.
F. Göbel, Ch. Mundt: Implementation of the P1 radiation model in the CFD solver NSMB and investigation of radiative heat transfer in the SSME main combustion chamber, AIAA-2011-2257, 17. AIAA Int. Space Planes and Hypersonic Systems and Technologies Conf., 2011.
S. Hatzl, T. Sander, Ch. Mundt: One-dimensional measurements of high enthalpy flow temperature using spontaneous Raman spectroscopy, AIAA-2011-2212, 17. AIAA Int. Space Planes and Hypersonic Systems and Technologies Conf., 2011.
D. Kliche, Ch. Mundt, E.H. Hirschel: The hypersonic Mach number independence principle in the case of viscous flow, Shock Waves, vol. 21, pp. 307-314, 2011.
Ch. Mundt, P. Altenhöfer: Results of HELM in initial operation as a shock tube, 11th Int. workshop on shock tube technology, Brisbane, 2011.
A. Sventitskiy, Ch. Mundt: Effect of the infrared emission properties from full-scale exhaust plumes, Int. Rev. Mech. Eng., vol. 4, no. 4, pp. 425-432, 2010.
P. Altenhöfer, Ch. Mundt: Comparison of L1d simulations with measurements on a double-diaphragm shock tube, EFMC8, 2010.
Ch. Messe, D. Kliche, T. Wallmersperger, B. Kröplin, Ch. Mundt: Modelling and Simulation of heat trnsfer on functionally gradedmaterials for hot structures in scramjet engines, submitted to 10. AIAA/ASME Thermophysics and heat transfer Conf., 2010.
S. Hatzl, T. Sander, Ch. Mundt: Measurements of high enthalpy flow temperature using a one-dimensional spontaneous Raman spectroscopy procedure, submitted to 27. AIAA Aerodynamic measurement and ground testing conference, 2010.
G. Schlöffel, A. Eichborn, H. Albers, Ch. Mundt, F. Seiler, F. Zhang: Experiments on the effect of a shock wave on the ignition behaviour of aluminium particles in a shock tube, Combustion and Flame, vol. 157, no. 3, pp. 446-454, 2010.
D. Kliche, Ch. Mundt: 1d supersonic combustor modelling, Australian Comb. Symp. II.3.3., 2009.
A. Thellmann, Ch. Mundt: CFD simulation of H2-O2 and CH4-O2 rocket combustion chamber including radiative effects, Australian Comb. Symp. II.3.1, 2009.
D. Kliche, Ch. Mundt: Combustor modelling for multidisciplinary analysis and evaluation of supersonic combustion ramjets, AIAA-2009-7282, 16. AIAA Int. Space Planes and Hypersonic Systems and Technologies Conf., 2009.
D. Kliche, Ch. Mundt, E.H. Hirschel: The hypersonic Mach number independence principle for inviscid and viscous flow, 27. Int. Symp. Shock Waves, paper 30474, 2009.
G. Schlöffel, H. Albers, F. Seiler, F. Zhang, Ch. Mundt: Effects of a shock wave on the morphology of aluminium particles, 27. Int. Symp. Shock Waves, paper 30537, 2009.
N. Reuß, Ch. Mundt: Experimental investigations of pressure distortions on the unsteady behaviour of a high pressure compressor, accepted for publication in AIAA Journ. Prop. Power, , vol. 25, no. 3, pp. 653-667, 2009.
G. Schlöffel, M. Bastide, S. Bachmann, Ch. Mundt, F. Seiler: Investigation of the Acceleration of Aluminium Particles behind a shock wave using instantaneous Laser Doppler Velocimetry, Shock Waves, vol. 19, pp. 125-134, 2009.
H. Griebel, B. Häusler, Ch. Mundt, H. Rapp, H.-J. Gudladt, M. Zähringer: The hypersonic drag balloon project Archimedes - a novel atmospheric sounding probe for Mars, Memoirs of the scientific sections of Academia Romana, pp. 159-182, 2008.
A.Sventitskiy, Ch. Mundt: Effect of nozzle exit shape on the infrared emissions of exhaust plumes, submitted to Aerospace Science and Technology, 2008.
A. Thellmann, Ch. Mundt: Modelling of Radiation Heat Transfer in Reacting Hot Gas Flows, 6th Eur. Symp. on Aerothermodynamics for Space Vehicles, 2008.
S. Hatzl, Ch. Mundt: Charakterisierung der spektralen Emissivität gespritzter keramischer Wärmedämmschichten, DLGR Jahrestagung Darmstadt, DGLR-JT2008-81251, 2008.
G. Schlöffel, M. Baside, Ch. Mundt, F. Seiler, J. Srulijes: Messung der Beschleunigung von Aluminium-Partikeln durch eine Stoßwelle mittels Laser-Doppler-Velozimetrie, , Lasermethoden in der Strömungsmeßtechnik, 2008.
K. Schemperg, Ch. Mundt: Study of numerical simulations for optimized operation of the free piston shock tunnel HELM, AIAA-2008-2653, 15. AIAA Int. Space Planes and Hypersonic Systems and Technologies Conf., 2008.
B. Thorwald, Ch. Mundt: Differential, analytical, second-order streamline-based solver for super- and hypersonic 2d-flows, AIAA-2008-2615, 15. AIAA Int. Space Planes and Hypersonic Systems and Technologies Conf., 2008.
D. Kliche, Ch. Mundt: Multidisciplinary analysis and evaluation of supersonic combustion ramjets, AIAA-2008-2602, 15. AIAA Int. Space Planes and Hypersonic Systems and Technologies Conf., 2008.
D. Kliche, R. Spieweg, R. Schweikhart, Ch. Mundt: Thrust reverser aerodynamic design: CFD analysis and comparison with experiments, CEAS-2007-451, Berlin, 2007.
H. Griebel, B. Häusler, Ch. Mundt, H. Rapp, H. Gudladt: The hypersonic drag balloon Archimedes and its research and testing program, CEAS-2007-358, Berlin, 2007.
K. Schemperg, Ch. Mundt: On the free piston shock tunnel at UniBwM (HELM), paper 2790 at the 26. Int. Symp. Shock Waves, 2007.
Ch. Mundt, R. Boyce, P. Jacobs, K. Hannemann: Validation study of numerical simulations by comparison to measurements in piston driven shock-tunnels, Aerospace Science and Technology vol. 11, iss. 2-3, pp.100-109, 2007.
Ch. Mundt, H. Griebel: Venus Balloon mission Archimedes-V with emphasis on surface and gas radiation phenomena, 1st Int. ARA conference, 2006.
S. G. Scheidler, S. Bindl, Ch. Mundt: Mapping the control parameters of an analogue fuel control to prepare for the retrofit of a digital control unit, ASME Turbo Expo 2006, GT-2006-90126, 2006.
H. Griebel, B. Häusler, Ch. Mundt, H. Rapp: Proposal for a Venus balloon entry probe (ARCHIMEDS-V) for studies of the atmosphere of Venus, Venus Entry Probe Workshop, ESTEC, The Netherlands, 2006.
B. Thorwald, Ch. Mundt: Neuer Lösungsansatz für Über-/Hyperschallströmungen, 12. STAB workshop, 2005.
A. Thellmann, Ch. Mundt, C. Welch, C. Jack: Entry of a solar kite into a planetary atmosphere, IAC-05-D.2.3, Fukuoka, 2005.
S. G. Scheidler, Ch. Mundt: Fatal damage of a twin-spool turbofan engine due to fan blade off, ISABE 2005-1206, 17. ISABE Konferenz München, 2005.
Ch. Mundt, H. Griebel, C. Welch: Studies of atmospheric entry of vehicles with very low ballistic coefficient, AIAA-2005-3384, AIAA/CIRA 13th Int. Space Planes and Hypersonic Systems and Technologies Conf., 2005.
Ch. Mundt: On the aerothermodynamic design of a piston-driven shock-tunnel, 9. International work shop on Shock tube technology, Woomera, 2004.
D. Kliche, R. Boyce, Ch. Mundt: Numerical calibration of the T-ADFA shock tunnel, 9. International work shop on Shock tube technology, Woomera, 2004.
N. Reuss, Ch. Mundt: Experimentelle Untersuchungen zum Einfluss kombinierter Eintrittstotaldruckstörungen auf das Betriebsverhalten des fünfstufigen Hochdruckverdichters Rig212, DGLR-Jahrestagung Dresden, Beitrag DGLR-JT2004-122, 2004.
H.Griebel, B.Häusler, Ch.Mundt, H.Rapp: Project ARCHIMEDES A Novel Approach to Balloon Deployment on Mars, IAC-04-Q.P.02, Vancouver, 2004.
K. Schemperg, Ch. Mundt: Zur gasdynamischen Auslegung eines Stoßwellenkanals, Vortrag GAMM 2004, Sektion Gasdynamik und hochverdünnte Gase, PAMM vol. 4, iss. 1, 2004.
S.G. Scheidler, Ch. Mundt, M. Mettenleiter, J. Hermann, S.-J. Hiller: Active stability control of the compression system in a twin-spool turbofan engine by air injection, 10. ISOMAC Symp., paper 10-2004-73, 2004.
H.S. Griebel, B. Häusler, Ch. Mundt: Die Mission ARCHIMEDES – ein Forschungsballon für den Mars und ein Technologieträger für die Zukunft, DGLR-Jahrestagung München, Beitrag DGLR-JT2003-258, 2003.
Ch. Mundt, P. Jacobs, R.R. Boyce, K. Hannemann: A comparative study of piston-driven shock-tunnels, DGLR-Jahrestagung München, Beitrag DGLR-JT2003-74, 2003.
Ch. Mundt, J. Lieser: Performance improvement of propulsion systems by optimization of the mixing efficiency and pressure loss of forced mixers, 8. CEAS European Propulsion Forum, Nottingham, 2001.
J. Lieser, R. Wilhelm, Ch. Mundt: Aerodynamischer Entwurf und Integration von Triebwerksgondeln bei Rolls-Royce Deutschland, DGLR-Jahrestagung Leipzig, Beitrag DGLR-JT2000-183, 2000.
Ch. Mundt: Realgaseffekte, Vortrag GAMM 2000, Sektion 24, Göttingen, 2000.
J. Lieser, Ch. Mundt: Aeroakustische Untersuchungen von Strahlmischern, STAB Workshop, DLR Göttingen, 1999.
M. Wegner, J. Lieser, Ch. Mundt: Lärm- und leistungsoptimierter Strahlmischer, DGLR-Jahrestagung Berlin, Beitrag DGLR-JT99-82, 1999.
Ch. Mundt, M. Wegner: Improvement of forced mixing in turbofan engines with respect to both noise and performance, 7. CEAS European Propulsion Forum, Pau, 1999.
R.R. Boyce, J.W. Morton, A.F.P Houwing, Ch. Mundt, D.J. Bone: Computational Fluid Dynamics Validation Using Multiple Interferometric Views of a Hypersonic Flowfield, Jour. Spacecraft & Rockets vol.33, no.3, pp.319-325, 1996.
Ch. Mundt, R.R. Boyce, E.H. Hirschel: Simulation of hypersonic, reacting flow around reentry bodies - Comparisons of numerical and experimental results, Z. Flugwiss. Weltraum- forsch. Bd.19, pp.492-501, 1995.
R.R. Boyce, F. Houwing, Ch. Mundt, J. Morton: CFD validation of real gas air flows over a blunt body using multiple interferometric views, AIAA-paper 94-2599, 1994.
A. Vinckier, R. Höld, Ch. Mundt, S.Wagner: Ein Viscous Shock Layer Verfahren für Hyperschallströmungen, Z. Flugwiss. Weltraumforsch. Bd. 18, pp.203-211, 1994.
R.R. Boyce, J. Morton, A.F.P. Houwing, Ch. Mundt, D. Bone: CFD validation using multiple interferometric views of three dimensional shock layer flows over a blunt body, AIAA paper 94-282, 1994.
Ch. Mundt, F. Monnoyer, R. Höld: Computational simulation of the aerothermodynamic characteristics for the reentry of HERMES, AIAA paper 93-5069, 1993.
S. Menne, G. Hartmann, F. Monnoyer, Ch. Mundt: Beiträge der DASA München zur nume- rischen Aerothermodynamik im HERMES Programm, DGLR Jahrestagung Göttingen, Beitrag Nr. 93-319, 1993.
D.J. Sutton, A.F.P. Houwing, P.C. Palma, R.R. Boyce, R.J. Sandeman, Ch. Mundt: The appli- cation of Laser Induced Fluorescence to the measurements of vibrational temperatures in a shock layer, AIAA paper 93-3071, 1993.
R. R. Boyce, D.R.N. Pulford, A.F.P. Houwing, Ch. Mundt, R. Sandeman: Comparison of non- equilibrium chemistry CFD calculations with broadband CARS measurements of local tem- peratures in hypervelocity nitrogen blunt body flows, Proc. 19. Int. Symp. Shock Waves, Marseille, 1993.
Ch. Mundt, R.R. Boyce, E.H. Hirschel: Simulation of hypersonic reacting flow around reentry bodies - Comparisons of numerical and experimental results, DGLR Jahrestagung Bremen, Beitrag Nr. 92-03-108, 1992.
Ch. Mundt, C. Weiland, E.H. Hirschel: How to use high enthalpy windtunnels in hypersonic design work?, Vortrag Euromech. Coll. 296 on Real gas effects in high enthalpy flows, Göttingen, 1992.
Ch. Mundt: Rechnerische Simulation reibungsbehafteter Strömungen im chemischen Nichtgleichgewicht, Dissertation Techn. Universität München, 1992.
Ch. Mundt: Calculation of hypersonic, viscous non-equilibrium flows around reentry bodies using a coupled Euler/boundary layer method, AIAA-paper 92-2856, 1992.
Ch. Mundt: Calculation of non-equilibrium flow past reentry vehicles, Vortrag Euromech. Coll. 289 on hypersonic aerodynamics, Aachen, 1992.
Ch. Mundt: Calculation of hypersonic flows in chemical non-equilibrium, Proc. 9. GAMM Conf. Num. Meth. Fl. Mech., J.B. Vos, A. Rizzi, I.L. Ryhming (eds.): Notes on Num. Fluid Mech. Bd. 35, pp.491-500, Vieweg Verl., Braunschweig, 1992.
R.R. Boyce, Ch. Mundt: Computational fluid dynamics code validation using a free piston hypervelocity shock tunnel, Proc. Int. Symp. Shock Waves, Sendai, Japan, 1991.
Ch. Mundt, E.H. Hirschel: Modelling of chemical and physiacl effects with respect to flows around reentry bodies, 3. Aerospace Symp. Braunschweig, 1991, H. Örtel, H. Körner (eds.): Orbital transport - Technical, meteorological, and technical aspects, Springer Verl., Berlin,
M.A. Schmatz, R.K. Höld, F. Monnoyer, Ch. Mundt, K.M. Wanie: Numerical methods for aerodynamic design II, Proc. Space Course on Low Earth Orbit Transportation and Orbital Systems, RWTH Aachen, Beitrag 62, 1991.
R.R. Boyce, Ch. Mundt: Aeronautical CFD studies of reentry flows, Conf. Proc. International Aerospace Congress, Bd. 3, pp.23-31, Melbourne, 1991.
Ch. Mundt, F. Monnoyer: Calculation of hypersonic non-equilibrium viscous flow using second-order boundary layer theory, Conf. Proc. International Aerospace Congress, Bd. 2, pp.425-432, Melbourne, 1991.
Ch. Mundt, R. Keraus, J. Fischer: New, accurate, vectorized approximations of state surfaces for the thermodynamic and transport properties of equilibrium air, Z. Flugwiss. Weltraum- forsch. Bd. 15, pp.179-185, 1991.
F. Monnoyer, Ch. Mundt, M. Pfitzner: Calculation of the hypersonic viscous flow past reentry vehicles with an Euler-boundary layer coupling method, AIAA-paper 90-417, 1990.
Ch. Mundt, M. Pfitzner, M.A. Schmatz: Calculation of viscous hypersonic flows using a coupled Euler/second-order boundary-layer method, Proc. 8. GAMM Conf. Num. Meth. Fl. Mech., P. Wesseling (ed.): Notes on Num. Fluid Mech. Bd. 29, pp.419-429, Vieweg Verl., Braunschweig, 1990.
