Dr.-Ing. Daniel Kliche


Dr.-Ing. Daniel Kliche
IABG mbH

 


Telefon: +49 89 6088 3976
eMail: daniel.kliche@unibw.de


Forschung...

Multidisziplinäre Analyse und Bewertung von Staustrahlantrieben mit Überschallverbrennung


Veröffentlichungen...

D. Kliche: Multidisziplinäre Analyse und Bewertung von Staustrahlantrieben mit Überschallverbrennung, Dissertation Universität der Bundeswehr München, 2012, ISBN 978-3-8439-0443-8.

Dissertation erhältlich im Verlag Dr. Hut unter der ISBN 978-3-8439-0443-8

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.

D. Kliche, Ch. Mundt: Progress in Multidisciplinary Analysis and Evaluation of Supersonic Combustion Ramjets, 17th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, San Francisco, California, April 11-14, 2011, AIAA-2011-2281.

Ch. Messe, D. Kliche, T. Wallmersperger, B. Kröplin, Ch. Mundt: Modeling and Simulation of Heat Transfer on Functionally Graded Materials for Hot Structures in Scramjet Engines, 10th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, Chicago, Illinois, USA, June 28-01, 2010, AIAA-2010-4896.

D. Kliche, Ch. Mundt: 1D Supersonic Combustor Modelling, Australian Combustion Symposium, Brisbane, Australia, December 02-04, 2009.

D. Kliche, Ch. Mundt: Combustor Modelling for Multidisciplinary Analysis and Evaluation of Supersonic Combustion Ramjets, 16th AIAA/DLR/DGLR International Space Planes and Hypersonic Systems and Technologies Conference, Bremen, Germany, October 19-22, 2009, AIAA-2009-7282.

D. Kliche, Ch. Mundt, E. H. Hirschel: The Hypersonic Mach Number Independence Principle in Case of Viscous Flow, 27th International Symposium on Shock Waves, St. Petersburg, Russia, July 19-24, 2009.

D. Kliche, M. Strohal, Ch. Mundt: Multidisciplinary Analysis and Evaluation of Supersonic Combustion Ramjets, 15th AIAA/AHI International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, Ohio, USA, April 28-01, 2008, AIAA-2008-2602.

D. Kliche, R. Spieweg, R. Schweikhart, Ch. Mundt: Thrust Reverser Aerodynamic Design: CFD Analysis and Comparison with Experiments, 1st CEAS European Air and Space Conference, Berlin, Germany, 2007, CEAS-2007-451.

D. Kliche, R. Boyce, Ch. Mundt: Numerical Calibration of the T-ADFA Shock Tunnel, 9th International Work Shop on Shock Tube Technology, Woomera, Australia, 2004.