## Publications

Google Scholar Researchgate Bibtex

#### Published / Accepted

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*, 113:231-249, 2019 [article]

D.T. Banuti, M. Grabe, K. Hannemann: “Flow characteristics of monopropellant micro-scale planar nozzles”, *Aerospace Science and Technology,* 86:341-350, 2019
[article]

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 *95:052120, 2017
[article]

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 (NNFM) *112:1–8, 2010

#### Selected Proceedings / Reports

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]

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]

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]

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]

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
[paper]

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]

#### Conference Proceedings

[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

[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“, 7*th 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

[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

[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”, 5*2nd 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” *19 ^{th}
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.

[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