Publications
Google Scholar Researchgate Bibtex
Journal Articles
G. Indelicato et al.
"Dataset of wall-resolved large eddy simulations turbulent pseudo-boiling in cryogenic hydrogen pipe flows"
Journal of Thermophysics and Heat Transfer
N.P. Longmire, D.T. Banuti
"Onset of heat transfer deterioration caused by pseudo-boiling in CO2 laminar boundary layers"
International Journal of Heat and Mass Transfer
D.T. Banuti
"The hybrid ergodic lattice gas model for critical fluids and the molecular nature of the critical point"
The Journal of Supercritical Fluids
J.A.A. Herrera, T. Hädrich, W. Pałubicki, D.T. Banuti, S. Pirk, D.L. Michels
"Weatherscapes: nowcasting heat transfer and water continuity"
ACM Transactions on Graphics (TOG)
T. Hädrich, D.T. Banuti, W. Pałubicki, S. Pirk, D.L. Michels
"Fire in paradise: mesoscale simulation of wildfires"
ACM Transactions on Graphics (TOG)
F. Maxim, K. Karalis, P. Boillat, D. T. Banuti, J. I. Marquez, B. Niceno, C. Ludwig, "Thermodynamics and Dynamics of Supercritical Water Pseudo‐Boiling" Advanced Science
T. Hädrich, M. Makowski, W. Pałubicki, D. T. Banuti, S. Pirk, and D. L. Michels.
"Stormscapes: Simulating Cloud Dynamics in the Now." ACM Transactions on Graphics
S. K. Beinke, J. S. Hardi, D.T. Banuti, S. Karl, B. B. Dally and M. Oschwald “Experimental and numerical study of transcritical oxygen-hydrogen rocket flame response to transverse acoustic excitation”, Proceedings of the Combustion Institute,
D.T. Banuti, M. Raju, M. Ihme: “Between supercritical liquids and gases – Reconciling dynamic and thermodynamic state transitions”, The Journal of Supercritical Fluids,
P.C. Ma, H. Wu, D.T. Banuti, M. Ihme: “Assessment of numerical schemes using diffuse interface methods for transcritical real-fluid simulations”, International Journal of Multiphase Flow
D.T. Banuti, M. Grabe, K. Hannemann: “Flow characteristics of monopropellant micro-scale planar nozzles”, Aerospace Science and Technology,
D.T. Banuti: (invited) “The latent heat of supercritical fluids”, Periodica Polytechnica Chemical Engineering, 63(2), pp. 270-275, 2019 [article]
S. Beinke, D. Banuti, J. Hardi, M. Oschwald, and B. Dally: “Modelling of a coaxial LOx/GH2 injection Progress in Propulsion Physics, 11:225-246, 2019 [article]
H. Riedmann, D. Banuti, B. Ivancic, O. Knab, K. Hannemann: „Modeling of H2/O2 single-element rocket thrust chamber combustion at sub- and supercritical pressures with different CFD tools”, Progress in Propulsion Physics, 11:247-272, 2019 [article]
D.T. Banuti, P.C. Ma, J.-P. Hickey, M. Ihme: “Thermodynamic structure of supercritical LOX-GH2 diffusion flames”, Combustion and Flame, 196:364-376, 2018 [article]
D.T. Banuti,
M. Raju, M. Ihme: “Similarity law for Widom- and coexistence lines”, Physical
Review E
M. Raju, D.T. Banuti, P.C. Ma, M. Ihme: “Widom lines in binary mixtures of supercritical fluids”, Nature Scientific Reports ,7:3027, 2017 [article]
D.T. Banuti, V. Hannemann, K. Hannemann. B. Weigand: “An efficient multi-fluid-mixing model for real gas reacting flows in liquid propellant rocket engines ”, Combustion and Flame 168:98–112, 2016 [article]
D.T. Banuti, K. Hannemann: “The absence of a dense potential core in supercritical injection: A thermal break-up mechanism”, Physics of Fluids 28:035103, 2016 [article]
D.T. Banuti: “Crossing the Widom line – supercritical pseudo-boiling”, Journal of Supercritical Fluids 98:12-16, 2015 [article] [preprint]
D.T. Banuti
and K. Hannemann: "Interfacial area transport equation in statistical-Eulerian-Eulerian simulations of multiphase flow. " Notes on Numerical Fluid
Mechanics and Multidisciplinary Design
Conference Proceedings
[38] B. D. Pena and D. T. Banuti, "Reinforcement learning for pathfinding with restricted observation space in variable complexity environments", AIAA Aerospace Sciences Meeting AIAA 2021-1755, Virtual, 2021
[37] N. P. Longmire and D. T. Banuti: "Modeling of the Supercritical Boiling Curve by Forced Convection for Supercritical Fluids in Relation to Regenerative Cooling", AIAA Aerospace Sciences Meeting AIAA 2021-1406, Virtual, 2021
[36] D. T. Banuti: "A critical assessment of adaptive tabulation for fluid properties using neural networks", AIAA Aerospace Sciences Meeting, Virtual, 2021
[35] D.T. Banuti: “Limitations of real fluid equations of state in computational fluid dynamics of direct-fired sCO2 cycles”, 7th International Supercritical CO2 Power Cycles Symposium, 2020
[34] D.T. Banuti and J. Bellan: “Inter-species molecular attraction effect in the development of a two-species mixing layer“, AIAA Science and Technology Forum and Exposition, 2020
[34] D.T. Banuti: “A thermodynamic look at injection in aerospace propulsion systems“, AIAA Science and Technology Forum and Exposition, 2020
[33] D. T. Banuti: ”Thermodynamic characterization of combustion systems”, 2019 Fall Meeting of the Western States Section of The Combustion Institute, 2019
[32] D. T. Banuti and J. Bellan: ”Influence of the real-gas equation-of-state binary interaction coefficients on the turbulent mixing of many species at diesel-engine high-pressure conditions”, 11th US National Combustion Meeting, 2019
[31] S. K. Beinke, J. S. Hardi, M. Oschwald, D.T. Banuti, S. Karl, B. Dally: “Analysis of Flame Response to Transverse Acoustic Velocity Forcing”, AIAA Joint Propulsion conference, 2018
[30] D.T. Banuti, D. Kim, S. Bose, L. Shunn: “Large-eddy simulations of oxy-fuel combustors for direct-fired supercritical CO2 power cycles”, 6th International Supercritical CO2 Power Cycles Symposium, 2018, [paper]
[29] P.C. Ma, H. Wu, D.T. Banuti, M. Ihme: “Assessment of diffused interface methods for transcritical real-fluid simulations“, AIAA Science and Technology Forum and Exposition, 2018
[28] B. Wagner et al.: “Rocket Propulsion in TAU: An Overview of the DLR ProTAU Project“, 7th European Conference for Aeronautics and Space Sciences, Milano, Italy, 2017
[27] D.T. Banuti, P.C. Ma, M. Ihme: “Phase separation analysis in supercritical injection using large-eddy-simulation and vapor-liquid-equilibrium”, AIAA 2017-1106, 2017, [paper]
[26] D.T. Banuti, M. Raju, P.C. Ma, M. Ihme, J.-P. Hickey: “Seven questions about supercritical fluids - towards a new fluid state diagram”, AIAA Science and Technology Forum and Exposition, Grapevine, USA, 2017, [paper]
[25] P.C. Ma, D.T. Banuti, M. Ihme, and J.-P. Hickey: “Numerical framework for transcritical real-fluid reacting flow simulations using the flamelet progress variable approach”, AIAA Science and Technology Forum and Exposition, Grapevine, USA, 2017
[24] D. Banuti, J.-P. Hickey, and M. Ihme “Sub- or supercritical? A flamelet analysis of high pressure rocket propellant injection”, 52nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Salt Lake City, USA, 2016
[23] J.-P. Hickey, P.C. Ma, D. Banuti, and M. Ihme: “Pseudo-phase change in transcritical combustion for liquid rocket engines”, Proceedings of Combustion Institute – Canadian Section Spring Technical Meeting, Waterloo, Canada, 2016
[22] H. Riedmann, D. Banuti, B. Ivancic, O. Knab, K. Hannemann: “Modeling of H2/O2 Single-Element Rocket Thrust Chamber Combustion at Sub- and Supercritical Pressures with Different CFD Tools”, 6th European Conference for Aeronautics and Space Sciences, Krakow, Poland, 2015
[21] S. Beinke, D. Banuti, J. Hardi, M. Oschwald, B. Dally: “Modelling of a Co-axial LOx/GH2 Injection Element Under High Frequency Acoustic Disturbances”, 6th European Conference for Aeronautics and Space Sciences, Krakow, Poland, 2015
[20] D. Saile, D. Banuti et al.: “Design of a Hot Plume Interaction Facility at DLR Cologne”, 8th European Symposium on Aerothermodynamics for Space Vehicles, Lisbon, Portugal, 2015
[19] S. Beinke, D. Banuti, J. Hardi, M. Oschwald, and B. Dally: ”Modelling an Acoustically Perturbed Rocket Engine Combustion Chamber with Cryogenic Propellant Injection” 19th Australasian Fluid Mechanics Conference, Melbourne, Australia, 2014
[18] D.T. Banuti and K. Hannemann: “Application of a Real-Gas-Library Multi-Fluid-Mixing Model to Supercritical Single Injector Flow’’ 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, USA, 2014
[17] D.T. Banuti and K. Hannemann: “Supercritical Pseudo-Boiling and its Relevance for Transcritical Injection’’ 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, USA, 2014
[16] D.T. Banuti, M. Grabe, and K. Hannemann: “Flow Characteristics of Micro-Scale Planar Nozzles’’ 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, Cleveland, USA, 2014
[15] D.T. Banuti and K. Hannemann: “Efficient multiphase rocket propellant injection model with high quality equation of state”, 4th Space Propulsion Conference, Cologne, Germany, 2014
[14] D.T. Banuti, M. Grabe, and K. Hannemann: “Planar Micro Nozzles – CFD Model Demands for Thrust Optimization”, 4th Space Propulsion Conference, Cologne, Germany, 2014
[13] M. Gauer, D. Banuti, D. Telitschkin, U. Gotzig, Y. Batonneau, P. Rangsten, M. Ivanov, P. Palmer, and R. Wiegerink: “PRECISE - Results of the MEMS µChemical Propulsion System.“ 4th Space Propulsion Conference, Cologne, Germany, 2014.
[12] S. Beinke, D. Banuti, J. Hardi and M. Oschwald: “HF-6 Testcase: LOX/H2-Combustion under forced acoustic excitation”. Proceedings of the REST Workshop, Vernon, France, 2014
[11] D.T. Banuti and K. Hannemann. “Real gas library in continuous phase propellant injection model for liquid rocket engines.” 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA 2013-4068, San Jose, USA, 2013.
[10] D.T. Banuti and K. Hannemann. “Steady Shock Refraction in Hypersonic Ramp Flow.” In Proceedings of the 17th AIAA International Space Planes and Hyper sonic Systems and Technologies Conference, AIAA 2011-2215, San Francisco, USA, 2011, [paper]
[9] D.T. Banuti and K. Hannemann. “Thermodynamic interpretation of cryogenic injection experiments.” 47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA 2011-5620, San Diego, USA, 2011.
[8] D.T. Banuti and K. Hannemann. “Effect of injector wall heat flux on cryogenic injection.” 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, AIAA 2010-7139, Nashville, USA, 2010.
[7] D.T. Banuti and K. Hannemann. “Flow control by energy deposition in hypersonic flow - some fundamental considerations.” In Proceedings of the 16th AIAA/DLR/DGLR International Space Planes and Hyper- sonic Systems and Technologies Conference, AIAA-2009-7345, Bremen, Germany, 2009. AIAA/DLR/DGLR
[6] D.T. Banuti, K. Hannemann, and J. Longo: “Aspects of Thermal Flow Control in Hypersonic Flight.” In Proceedings of the CEAS Air and Space Conference, Manchester, UK, 2009.
[5] J.M.A. Longo, R. Dittrich, D. Banuti, M. Sippel, J. Klevanski, U. Atanassov, G. Carrier, Ph. Duveau, I. Salah El Din, R. Thepot, A. Loubeau, F. Coulouvrat, R. Jarlas, H. Rabia, D. Perigo, and J. Steelant: “Concept Study for a Mach 6 Transport Aircraft.” AIAA-2009-435, 2009
[4] D. Banuti, K. Hannemann: “Interfacial Area Transport Equation in Statistical-Eulerian-Eulerian Simulations of Multiphase Flow.” 16. DGLR/STAB Symposium, Aachen, Germany, 2008.
[3] D. Banuti,
S. Karl, and K. Hannemann: “Interfacial Area Modeling for Eulerian Spray
Simulations in Liquid Rocket Engines.” AIAA-2008-5231, 2008.
[2] D. Banuti: “Entwurf von Vorkörpermodifikationen und Einfluß auf das Drucknahfeld eines Hyperschalltransportflugzeuges.” 13. STAB-Workshop, Göttingen, Germany, 2007.
[1] E. Jacob, G. Flandro, and D.T. Banuti:
“Forced Resonant Shock Waves and Mean Pressure Shift in a Closed Tube.”
AIAA-2007-5806, 2007.
Other conferences
D.T. Banuti, D. Kim, S. Bose, L. Shunn: “Large eddy simulation of a direct-fired sCO2 combustor", Poster, University Turbine Systems Research (UTSR) Project Review Meeting, Pittsburgh 2017
D.T. Banuti, P.C. Ma, M. Raju, M. Ihme: “Interfacial and Bulk Thermodynamics in Supercritical Combustion”, 16th SIAM International Conference on Numerical Combustion, Orlando, 2017
S. Beinke, D.T. Banuti, J. Hardi, S. Karl, M. Oschwald, D. Dally: “Modelling of a Coaxial LOX/GH2 Injection Element under High Frequency Transverse Acoustic Velocity Forcing”, 16th SIAM International Conference on Numerical Combustion, Orlando, 2017
P.C. Ma, Y. Lv, D.T. Banuti, J.-P. Hickey, M. Ihme: “Numerical methods for transcritical real-fluid reacting flows using the flamelet progress variable approach” 16th SIAM International Conference on Numerical Combustion, Orlando, 2017
D.T. Banuti, M. Raju, J.P. Hickey, M. Ihme: “The latent heat of vaporization of supercritical fluids”, APS-DFD Meeting, Portland, USA, 2017
P. Govindaraju, P.C. Ma, D.T. Banuti, M. Ihme: “High-pressure mixing of liquid dodecane in a nitrogen environment” APS-DFD Meeting, Portland, USA, 2017
D. Banuti, K. Hannemann: “The absence of a dense potential core in transcritical injection”, 15th International Conference on Numerical Combustion, Avignon, France 2015.
D. Banuti, S. Beinke, E. Costa Ruiz, T. Eggers, C. Génin, P. Gerlinger , K. Hannemann, S. Jack, S. Karl, M. Oschwald, M. Rudolph, K. Schäfer, D. Schneider, M. Seidl, D. Suslov, B. Wagner: “Rocket Propulsion in TAU: An Overview of Rocket Propulsion Modeling with the DLR TAU code” (in German), Congress of the German Aerospace Society DGLR, Rostock, Germany, 2015
Technical reports
D.T. Banuti, J. O’Brian, Lee Shunn: “Highly scalable large-eddy simulations of oxy-fuel combustors for direct-fired supercritical CO2 power cycles”, DOE SBIR, 2018
D.T. Banuti, M. Raju, M. Ihme: “On the characterization of transcritical fluid states”, CTR Research Briefs, Stanford University, 2017 [report]
D.T. Banuti, M. Raju, M. Ihme: “Supercritical pseudoboiling for general fluids and its application to injection”, CTR Research Briefs, Stanford University, 2016 [report]
D.T. Banuti: “Thermodynamic analysis and numerical modeling of supercritical injection”, DLR FB 2015-16, 2015
D.T. Banuti: “Description of real gas modeling in TAU” Technical Report B2.1; DLR Project ProTAU, 2014
D.T. Banuti: “Comparison of experimental and numerical results’’ Technical Report D5.508 ESA 7th FP PRECISE 2014
D.T. Banuti: “Wind-tunnel aerothermodynamic design’’ Technical Report ESA TRP-HOTP-DTN2500, 2013
D.T. Banuti: “Definition of Scaling Parameters’’ Technical Report ESA TRP-HOTP-DTN2200, 2012
M. Grabe and D.T. Banuti: “CFD roadmap’’ Technical Report D4.404 ESA 7th FP PRECISE, 2012
D.T. Banuti: “Hydrazine reaction kinetics in TAU’’ Technical Report D5.502 ESA 7th FP PRECISE, 2012
D.T. Banuti and M. Grabe: “Numerical modeling of a MEMS chemical propulsion system’’ Technical Report ESA GSTP-4 Task 7, 2010
D.T. Banuti: “Report on the assessment of the potential of plasma flow control devices for Mach 6 SST” Deliverable D.2.1.7 Contract No. AST5-CT-2006-030729, ATLLAS, 2010
D.T. Banuti and C. Böttcher: “Numerical Tool for Plasma Actuator Modelling.” Deliverable D.2.1.6 Contract No. AST5-CT-2006-030729, ATLLAS, 2009
D.T. Banuti: “Numerical Investigation of Aero-Spikes and Aero-Jet-Spikes for Mach 6 SST.” Deliverable D.2.1.5. Contract No. AST5-CT-2006-030729, ATLLAS, 2008
Theses
Dissertation: “Thermodynamic Analysis and Numerical Modeling of Supercritical Injection”, University of Stuttgart, 2015, Prof. Bernhard Weigand
MSc thesis (“Diplomarbeit”): "Blunt Body Near Wake Modelling and Pressure Interpolation on Immersed Boundaries using Vorticity Confinement." Aachen University, Prof. Norbert Peters / University of Tennessee Space Institute, Prof. John Steinhoff, 2006
Graduate research project (“Studienarbeit”): “Development of a Genetic Algorithm for approximation of premixed flame velocities” (in German), RWTH Aachen University, Prof. Norbert Peters, 2005
Graduate research project (“Studienarbeit”): “Development of a direct point extraction algorithm for automatic grid generators” (in German), Aachen University, Prof. Wolfgang Schröder, 2005