Presentation

Liquid and electric space propulsion

Open Access

Large-eddy simulation of trans- and supercritical injection p. 5

H. Müller, C. A. Niedermeier, M. Jarczyk, M. Pfitzner, S. Hickel and N. A. Adams

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608005

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Numerical simulations of mixing under supercritical pressures of a shear coaxial injector using a high-order method: effect of outer jet temperature p. 25

H. Terashima and M. Koshi

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608025

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Temperature measurement of cryogenic nitrogen jets at supercritical pressure p. 43

H. Tani, S. Teramoto, T. Toki, S. Yoshida, K. Yamaguchi and K. Okamoto

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608043

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Development of combustion response functions in a subscale high-pressure transverse combustor p. 55

M. Wierman, B. Pomeroy and W. Anderson

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608055

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Cryogenic oxygen jet response to transverse acoustic excitation with the first transverse and the first combined longitudinal-transverse modes p. 75

J. S. Hardi and M. Oschwald

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608075

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Investigation of different modeling approaches for computational fluid dynamics simulation of high-pressure rocket combustors p. 95

B. Ivancic, H. Riedmann, M. Frey, O. Knab, S. Karl and K. Hannemann

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608095

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Evolution of cooling-channel properties for varying aspect ratio p. 117

M. Pizzarelli, F. Nasuti and M. Onofri

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608117

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Numerical and experimental investigation of the methane film cooling in subscale combustion chamber p. 129

Y. Daimon, H. Negishi, M. Koshi and D. Suslov

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608129

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Injector characterization for a gaseous oxygen-methane single element combustion chamber p. 145

M. P. Celano, S. Silvestri, G. Schlieben, C. Kirchberger, O. J. Haidn and O. Knab

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608145

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Concept of electric propulsion realization for high power space tug p. 165

L. E. Zakharenkov, A. V. Semenkin and A. E. Solodukhin

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608165

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Solid and hybrid propulsion

Open Access

Contrail formation in the tropopause region caused by emissions from an Ariane 5 rocket p. 183

Ch. Voigt, U. Schumann and K. Graf

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608183

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Detailed analysis of a quench bomb for the study of aluminum agglomeration in solid propellants p. 197

S. Gallier, J.-G. Kratz, N. Quaglia and G. Fouin

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608197

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Analysis of pressure blips in aft-finocyl solid rocket motor p. 213

M. Di Giacinto, B. Favini and E. Cavallini

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608213

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A wide characterization of paraffin-based fuels mixed with styrene-based thermoplastic polymers for hybrid propulsion p. 241

M. Boiocchi, P. Milova, L. Galfetti, L. Di Landro and A. K. Golovko

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608241

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Rheological, optical, and ballistic investigations of paraffin-based fuels for hybrid rocket propulsion using a two-dimensional slab-burner p. 263

M. Kobald, E. Toson, H. Ciezki, S. Schlechtriem, S. di Betta, M. Coppola and L. DeLuca

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608263

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Theoretical prediction of regression rates in swirl-injection hybrid rocket engines p. 283

K. Ozawa and T. Shimada

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608283

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Scramjet and pressure-gain combustion

Open Access

Ignition length study of jp-8 + 100 in a supersonic duct p. 309

M. L. Bateup

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608309

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Conversion of hydrocarbon fuel in thermal protection reactors of hypersonic aircraft p. 321

A. L. Kuranov, A. M. Mikhaylov and A. V. Korabelnikov

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608321

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Specific features of ignition and flameholding of hydrocarbon fuels in high-speed flow p. 333

M. Goldfeld

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608333

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The role of presumed probability density functions in the simulation of nonpremixed turbulent combustion p. 353

A. Coclite, G. Pascazio, P. De Palma and L. Cutrone

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608353

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Three-dimensional numerical simulation of a continuously rotating detonation in the annular combustion chamber with a wide gap and separate delivery of fuel and oxidizer p. 375

S. M. Frolov, A. V. Dubrovskii and V. S. Ivanov

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608375

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Mathematical modeling of detonation initiation via flow cumulation effects p. 389

I. Semenov, P. Utkin and I. Akhmedyanov

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608389

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Gas turbine propulsion

Open Access

Testing and analysis of the impact on engine cycle parameters and control system modifications using hydrogen or methane as fuel in an industrial gas turbine p. 409

H. H.-W. Funke, J. Keinz, S. Börner, P. Hendrick and R. Elsing

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608409

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Open Access

Computational fluid dynamics / Monte Carlo simulation of dusty gas flow in a “rotor-stator” set of airfoil cascades p. 427

Yu. M. Tsirkunov and D. A. Romanyuk

Published online: 06 July 2016

DOI: https://doi.org/10.1051/eucass/201608427

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