Oliver Knab

发表

Modeling of H_2/O_2 Single-Element Rocket Thrust Chamber Combustion at Sub- and Supercritical Pressures with Different CFD Tools

Klaus Hannemann, Hendrik Riedmann, Daniel T. Banuti, 2015 .

Application of Astrium's CryoROC Code to a Single Injector Problem. A Contribution to the RCM-3 Mascotte Test Case (60 bar)

Oliver Knab, Josef Gorgen, 2001 .

Investigation of different modeling approaches for CFD simulation of high pressure rocket combustors

Klaus Hannemann, Sebastian Karl, Hendrik Riedmann, 2013 .

Simulation of a GOX–kerosene subscale rocket combustion chamber

Christoph Kirchberger, Hans-Peter Kau, Oliver Knab, 2011 .

Comparison of Single Element Rocket Combustion Chambers with Round an Square Cross Sections

Oskar Haidn, Oliver Knab, S. Silvestri, 2015 .

Investigation on Recess Variation of a Shear Coax Injector for a Single Element GOX/GCH4 Combustion Chamber

Oskar Haidn, Christoph Kirchberger, Oliver Knab, 2016 .

Film Cooling Investigations within a GOX/Kerosene Combustion Chamber

Christoph Kirchberger, Oliver Knab, Gregor Schlieben, 2011 .

TMF: Laser Application for a Close-to-Reality Simulation of Thermo-Mechanical Fatigue Processes in Rocket Engines

Andreas Gernoth, Jörg Riccius, Elena Suslova, 2007 .

Experimental and Numerical Film Cooling Investigations in a GOX/ Kerosene Rocket Combustion Chamber

Oskar Haidn, Christoph Kirchberger, Oliver Knab, 2014 .

Modeling and simulation of a GOX/kerosene subscale rocket combustion chamber with film cooling

Oskar Haidn, Christoph Kirchberger, Oliver Knab, 2015 .

Investigation of different modeling approaches for computational fluid dynamics simulation of high-pressure rocket combustors

Klaus Hannemann, Manuel Frey, Blazenko Ivancic, 2016 .

Advanced Cooling Circuit Layout for the VINCI Expander Cycle Thrust Chamber

Oliver Knab, Wolfgang Haslinger, Anton Fröhlich, 2002 .

Full-Scale Virtual Thrust Chamber Demonstrators as Numerical Testbeds within SFB-TRR 40

Hendrik Riedmann, Oliver Knab, Oskar J. Haidn, 2018, 2018 Joint Propulsion Conference.

Modeling of Rocket Combustion Devices

Blazenko Ivancic, Oliver Knab, Manuel Frey, 2010 .

Radiative heat transfer analysis in modern rocket combustion chambers

Christian Mundt, Oliver Knab, Manuel Frey, 2014 .

EFFECTIVE CALCULATION OF MULTIPHASE FLOW FIELDS IN LIQUID ROCKET THRUST CHAMBERS.

Oliver Knab, Dag Wennerberg, 2001 .