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Modeling of gas–surface interface for paraffin-based hybrid rocket fuels in computational fluid dynamics simulations p. 3

D. Bianchi, F. Nasuti and D. Delfini

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911003

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The HyEnD stern hybrid sounding rocket project p. 25

M. Kobald, C. Schmierer, U. Fischer, K. Tomilin, A. Petrarolo and M. Rehberger

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911025

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Effects of aluminum composites on the regression rates of solid fuels p. 65

C. Paravan, S. Penazzo, S. Dossi, M. Stocco, L.T. DeLuca and L. Galfetti

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911065

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Green gelled propellant highly throtteable rocket motor and gas generator technology: status and application p. 91

P. Caldas Pinto, H.K. Ciezki, K.W. Naumann, J. Ramsel, P. Kröger, H. Niedermaier, M. Negri, S. Scheutzow, A. Thumann and G. Kurth

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911091

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Mathematical modeling of agglomerates evolution p. 131

V.A. Babuk, N.L. Budnyi and A.A. Nizyaev

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911131

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Numerical analysis of combustion for droplet of hydrazine p. 149

M. Motoe

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911149

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Analytical viscous flow model and test validation of a swirl injector for rocket engine application p. 161

G. Fiore, C. Bach, J. Sieder and M. Tajmar

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911161

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Large-eddy simulation of transcritical liquid oxygen/methane jet flames p. 177

H. Müller and M. Pfitzner

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911177

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Eulerian coupling of two-phase flow models for the large eddy simulation of the atomization in cryogenic combustion chamber p. 195

A. Murrone and C. Le Touze

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911195

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Modeling of a coaxial liquid oxygen/gaseous hydrogen injection element under high-frequency acoustic disturbances p. 225

S. Beinke, D. Banuti, J. Hardi, M. Oschwald and B. Dally

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911225

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Modeling of H₂/O₂ single-element rocket thrust chamber combustion at sub- and supercritical pressures with different computational fluid dynamics tools p. 247

H. Riedmann, D. Banuti, B. Ivancic, O. Knab and K. Hannemann

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911247

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One-dimensional model describing eigenmode frequency shift during transverse excitation p. 273

S. Webster, J. Hardi and M. Oschwald

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911273

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Nonlinear analysis of low-frequency combustion instabilities in liquid rocket engines p. 295

M. Leonardi, F. Di Matteo, J. Steelant, F. Nasuti and M. Onofri

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911295

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Consequences of modeling demands on numerical rocket thrust chamber flow simulation tools p. 317

O. Knab, H. Riedmann, B. Ivancic, C. Höglauer, M. Frey and T. Aichner

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911317

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Numerical investigation of an unsteady injection adapted to the continuous detonation wave rocket engine operation p. 347

T. Gaillard, D. Davidenko and F. Dupoirieux

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911347

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Ballistic phase performance model for cold gas attitude control in cryogenic upper stages p. 371

M. Werner, S. Kottmeier, T. Bruns and N. Korus

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911371

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Hot-fire testing of liquid oxygen/hydrogen single coaxial injector at high-pressure conditions with optical diagnostics p. 391

D.I. Suslov, J.S. Hardi, B. Knapp and M. Oschwald

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911391

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Flame response to high-frequency oscillations in a cryogenic oxygen/hydrogen rocket combustor p. 407

N. Fdida, J. Hardi, H. Kawashima, B. Knapp, M. Oschwald and A. Ristori

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911407

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Measuring the phase between fluctuating pressure and flame radiation intensity in a cylindrical combustion chamber p. 425

S. Gröning, J.S. Hardi, D. Suslov and M. Oschwald

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911425

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Development of LM10-MIRA liquid oxygen – liquid natural gas expander cycle demonstrator engine p. 447

P. Bellomi, M. Rudnykh, S. Carapellese, D. Liuzzi, G. Caggiano, L. Arione, A.A. Gurtovoy, S.D. Lobov, V. S. Rachuk, E. D'Aversa et al. (2 more)

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911447

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LOx/ethanol gas generator: investigation and development p. 467

R.H.S. Hahn, L.B. Nascimento and D.S. Almeida

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911467

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VINCI^®, the european reference for ariane 6 upper stage cryogenic propulsive system p. 481

P. Alliot, J.-F. Delange, V. De Korver, J.-M. Sannino, A. Lekeux and B. Vieille

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911481

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Delivering engine demonstrators for competitive evolutions of the european launchers p. 495

J.-N. Caruana, M. De Rosa, T. Kachler, W. Schoroth and K. Underhill

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911495

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Design of an arc-based thrust-optimized nozzle contour p. 517

K. Schomberg, J. Olsen, A. Neely and G. Doig

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911517

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Shallow water experiments to verify a numerical analysis on an aerodynamically thrust-vectored aerospike nozzle p. 529

J. Sieder, M. Propst, C. Bach and M. Tajmar

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911529

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Parametrical study on side load generation in subscale rocket nozzles p. 543

R. Stark and C. Génin

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911543

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Experimental study of water hammer pressure surge p. 555

C. Bombardieri, T. Traudt and C. Manfletti

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911555

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A preliminary design study for an expander liquid oxygen turbopump p. 571

C. Maeding, L. Souverein, D. Hummel, S. Koenigbauer, A. Wagner and J. Alting

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911571

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Design and tool anchoring for a 120-kilonewton expander cycle rocket engine liquid oxygen turbopump p. 591

L. Souverein, C. Maeding, T. Aichner, B. Ivancic, A. Wagner and M. Frey

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911591

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Analytical models of unstable rarefied gas flow in channels and nozzles: simulation and comparison p. 613

O.A. Aksenova and I.A. Khalidov

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911613

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Numerical simulation of a backward-facing step combustor using reynolds-averaged navier–stokes / extended partially stirred reactor model p. 625

N. Petrova, V. Sabelnikov and N. Bertier

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911625

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Quasi-two-dimensional approximation for numerical simulation of flows in engine ducts p. 657

V. Vlasenko and A. Shiryaeva

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911657

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Experimental investigation of spray combustion regimes in aeroengine combustors p. 677

M. Vicentini, R. Lecourt, O. Rouzaud, V. Bodoc and O. Simonin

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911677

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Exploratory investigations on metal-based fuels for air-breathing propulsion p. 699

F. Maggi, S. Colciago, C. Paravan, S. Dossi and L. Galfetti

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911699

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Experimental investigation of the effect of the air inlet angle and the combustion pressure in a ducted rocket combustor p. 713

V. Laguzzi, F. Molinaro and B. Natan

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911713

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The numerical simulation techniques research and preliminary experimental validation of the start characteristics for a two-dimensional hypersonic inlet p. 729

A. Yu, D. Yang, J. Wu, H. Ni and J. Le

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911729

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Microvortex generator for scramjet inlet application p. 747

A.C. Idris, M.R. Saad and K. Kontis

Published online: 08 February 2019

DOI: https://doi.org/10.1051/eucass/201911747

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