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Chapter One. Turbulence modeling

Open Access

Comparative study of different turbulence modeling approaches to prediction of transonic and supersonic flows past a reentry capsule with balance flaps p. 3

A. Garbaruk, D. Niculin, M. Strelets, A. Dyadkin, A. Krylov and K. Stekenius

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305003

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Fine-tuning of DDES and IDDES formulations to the k-ω shear stress transport model p. 23

M. S. Gritskevich, A. V. Garbaruk and F. R. Menter

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305023

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Assessment of an approach to generating inflow synthetic turbulence for large eddy simulations of complex turbulent flows p. 43

D. Y. Adamian and A. K. Travin

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/20130543

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Chapter Two. Boundary layer stability

Open Access

Direct numerical simulations of mack-mode damping on porous coated cones p. 57

H. Lüdeke and V. Wartemann

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305057

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Open Access

Experiments on relative receptivity of three-dimensional supersonic boundary layer to controlled disturbances and its development p. 69

A. D. Kosinov, G. L. Kolosov, A. V. Panina, N. V. Semionov and Yu. G. Yermolaev

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305069

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Open Access

Experimental study of stability and transition of supersonic boundary layer on swept wing at mach number 2-4 p. 81

N. V. Semionov, A. D. Kosinov, Yu. G. Yermolaev and R. I. Kazantsev

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305081

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Open Access

Effects of shock on hypersonic boundary layer stability p. 93

F. Pinna and P. Rambaud

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305093

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Chapter Three. Flow control

Open Access

Arbitrary Lagrangian-Eulerian approach in reduced order modeling of a flow with a moving boundary p. 109

W. Stankiewicz, R. Roszak and M. Morzyński

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305109

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Open Access

A summary of laser and microwave flow control in high-speed flows p. 125

D. Knight

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305125

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Open Access

Flowfields around supersonic aerodynamic bodies under the action of asymmetric energy release p. 139

O. A. Azarova, D. Knight and Yu. F. Kolesnichenko

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305139

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Chapter Four. Vortex, wake, and base flows

Open Access

Stability of symmetric vortex flow over slender bodies and possibility of control by local gas heating p. 155

V. I. Shalaev and I. V. Shalaev

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305155

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Open Access

Base-flow sensitivity of a generic rocket forebody towards small freestream angles p. 169

C. C. Wolf, Y. You, R. Hörnschemeyer, H. Lüdeke and V. Hannemann

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305169

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Open Access

Numerical investigation of the near wake of generic space launcher systems at transonic and supersonic flows p. 191

V. Statnikov, C. Glatzer, J.-H. Meiß, M. Meinke and W. Schröder

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305191

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Investigations on the turbulent wake of a generic space launcher geometry in the hypersonic flow regime p. 209

D. Saile, A. Gülhan, A. Henckels, C. Glatzer, V. Statnikov and M. Meinke

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305209

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Experimental investigation on interstage thermal environment of launch vehicle with multijets in wind tunnel p. 235

J. Lin, C. Cao, Y. Wu and S. Zhang

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305235

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Chapter Five. Shock interaction

Open Access

Numerical analysis of three complex three-dimensional shock wave / turbulent boundary layer interaction flows p. 247

A. D. Grosvenor, A. A. Zheltovodov, M. A. Matheson, L. M. Sailer, M. Krzysztopik and D. P. Gutzwiller

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305247

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Open Access

Shock induced fluid-structure interaction on a flexible wall in supersonic turbulent flow p. 285

S. Willems, A. Gülhan and B. Esser

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305285

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Open Access

Large-eddy simulation of high mach number film cooling with shock-wave interaction p. 309

M. Konopka, M. Meinke and W. Schröder

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305309

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Open Access

Three-dimensional shock-wave/boundary-layer interaction at the presence of entropy layer p. 327

V. Borovoy, I. Egorov, A. Maximenko, V. Mosharov, V. Radchenko, A. Skuratov and I. Struminskaya

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305327

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Supersonic laminar separated flow structure at a ramp for a free-stream mach number of 6 p. 349

V. I. Zapryagaev, I. N. Kavun and I. I. Lipatov

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305349

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Open Access

Experimental and numerical study of dual bell nozzle flow p. 363

C. Génin, R. Stark, O. Haidn, K. Quering and M. Frey

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305363

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Chapter Six. Hypersonics

Open Access

Hypersonic boundary layer in the vicinity of a point of inflection of leading edge on a flat wing in the regime of strong viscous interaction p. 379

G. N. Dudin and A. V. Ledovskiy

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305379

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Open Access

Numerical analysis of dusty gas flow in a hypersonic shock tunnel p. 393

Yu. M. Tsirkunov and A. A. Verevkin

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305393

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Open Access

Delta wing with blunted leading edges at angle of attack in hypersonic flow p. 415

P. Vashchenkov, A. Kashkovsky and M. Ivanov

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305415

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Chapter Seven. Reentry

Open Access

Evaluation of the aerodynamic properties of the intermediate experimental vehicle in the rarefied and transitional regime p. 425

T. Bányai, E. Torres, T. E. Magin, A. V. Kashkovsky, P. V. Vashchenkov, M. S. Ivanov and P. Rambaud

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305425

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Open Access

Numerical investigation of two-phase flow structure and heat transfer in a supersonic dusty gas flow over a blunt body p. 441

B. Oesterle, A. N. Volkov and Yu. M. Tsirkunov

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305441

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Open Access

A novel kinetic model for chemical energy accommodation on silica surface p. 457

S. Di Benedetto and C. Bruno

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305457

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Open Access

Numerical simulations of supersonic flow past the Earth descent module for Phobos-grunt sample return mission p. 481

I. V. Egorov, D. V. Ivanov and A. V. Novikov

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305481

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Open Access

Nonequilibrium computational flowfield analysis for the design of mars manned entry vehicles p. 493

A. Viviani and G. Pezzella

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305493

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Chapter Eight. Real gases and rarefied flows

Open Access

Uncertainty quantification for characterization of high enthalpy facilities p. 519

N. Villedieu, J. Cappaert, J. P. Garcia Galache and T. E. Magin

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305519

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Open Access

Transport properties of partially ionized atomic gases with electronic excitation p. 533

V. A. Istomin and E. V. Kustova

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305533

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Open Access

Modeling Intermediate eXperimental Vehicle control thruster plume-surface interaction p. 545

A. V. Kashkovsky, P. V. Vashchenkov, T. Bányai and M. S. Ivanov

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305545

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Open Access

Experimental study of nonequilibrium dissociation of molecular oxygen p. 557

N. G. Bykova, L. B. Ibraguimova, O. P. Shatalov, Yu. V. Tunik and I. E. Zabelinskii

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305557

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Chapter Nine. Configuration aerodynamics, sonic boom, and aircraft aerodynamic model

Open Access

On optimal configurations in supersonic flow p. 571

V. I. Lapygin, T. V. Sazonova and G. E. Yakunina

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305571

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Open Access

Experimental research of the boundary layer structure at near-critical angles of attack for the classical and wavy wings p. 583

I. Zverkov, V. Kozlov and A. Kryukov

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305583

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Open Access

Impact of multipole matching resolution on supersonic aircraft sonic boom assessment p. 601

I. Salah El Din, M.-C. Le Pape, A. Minelli, R. Grenon and G. Carrier

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305601

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Open Access

Aerodynamic model development and simulation of airliner spin for upset recovery p. 621

A. Khrabrov, M. Sidoryuk and M. Goman

Published online: 14 June 2013

DOI: https://doi.org/10.1051/eucass/201305621

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