Presentation

Aerodynamics

Open Access

Dynamics of molecules in a supercooled water nanoparticle during the ice accretion on the aircraft surface p. 3

I. A. Amelyushkin and A. L. Stasenko

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507003

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Open Access

Helicopter fuselage drag ─ combined computational fluid dynamics and experimental studies p. 21

A. Batrakov, A. Kusyumov, S. Mikhailov, V. Pakhov, A. Sungatullin, M. Valeev, V. Zherekhov and G. Barakos

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507021

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Open Access

Aerodynamic performance of the DeSiReH high-lift laminar wing at free flight and ETW in-tunnel conditions p. 33

S. Bosnyakov, E. Kazhan, I. Kursakov, S. Matyash, S. Mikhaylov and A. Lysenkov

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507033

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Open Access

Calculations of unsteady flows around high-lift configurations based on a zonal approach p. 45

S. Bosnyakov, I. Kursakov, S. Mikhaylov and V. Vlasenko

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507045

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Open Access

Improvement of the cruise performances of a wing by means of aerodynamic optimization. Validation with a Far-Field method p. 67

J. Jiménez-Varona and J. Ponsin Roca

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507067

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Open Access

Calculation of tumbling boundaries of a generic wing-only airliner p. 89

A. Khrabrov and M. Sidoryuk

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507089

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Open Access

Aerodynamic analysis of a helicopter fuselage with rotating rotor head p. 99

R. Reß, M. Grawunder and Ch. Breitsamter

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507099

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Experimental facilities

Open Access

OFF-Stagnation point testing in plasma facility p. 113

A. Viladegut and O. Chazot

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507113

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Open Access

Experimental investigation of a newly designed supersonic wind tunnel p. 123

J. Wu and R. Radespiel

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507123

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Flow control

Open Access

The effects of actuation frequency on the separation control over an airfoil using a synthetic jet p. 147

Y. Abe, K. Okada, T. Nonomura and K. Fujii

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507147

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Open Access

On the possibility of laminar flow control on a swept wing by means of plasma actuators p. 169

S. L. Chernyshev, A. P. Kuryachii, S. V. Manuilovich, D. A. Rusyanov and V. V. Skvortsov

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507169

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Open Access

Investigation of flow separation control by nanosecond pulsed dielectric barrier discharge actuators p. 191

N. Grech, P. Leyland, Ph. Peschke and P. Ott

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507191

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Open Access

Instability wave control in turbulent jet by acoustical and plasma actuators p. 211

V. F. Kopiev, I. V. Belyaev, G. A. Faranosov, V. A. Kopiev, N. N. Ostrikov, M. Yu. Zaytsev, Yu. S. Akishev, M. E. Grushin, N. I. Trushkin, V. A. Bityurin et al. (5 more)

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507211

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Numerical and experimental investigation of slot-blown air over a cylinder p. 229

W. Runge, F. Buysschaert, J. Hayez, F. Carlier, H. Antoine, P. Hendrick, G. Dimitriadis and G. Degrez

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507229

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Inlets, nozzles, and internal flows

Open Access

Development of advanced computational fluid dynamics tools and their application to simulation of internal turbulent flows p. 247

V. N. Emelyanov, A. G. Karpenko and K. N. Volkov

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507247

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Flow separation in out-of-round nozzles, a numerical and experimental study p. 269

C. Génin, R. Stark and S. Jack

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507269

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Open Access

Analysis of the reverse jet influence on particle ingestion at the engine inlet p. 283

S. Yu. Krasheninnikov and D. E. Pudovikov

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507283

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Jets and wakes

Open Access

Experimental and numerical study of pulsating transversal jets p. 297

M. A. Goldfeld, N. N. Fedorova, I. A. Fedorchenko, G. A. Pozdnyakov, K. Yu. Timofeev and Yu. V. Zhakharova

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507297

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Combined experimental and numerical investigation of a transonic space launcher wake p. 311

S. Scharnowski, V. Statnikov, M. Meinke, W. Schröder and C. J. Kähler

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507311

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Experimental and numerical investigation of the turbulent wake flow of a generic space launcher configuration p. 329

V. Statnikov, D. Saile, J.-H. Meiß, A. Henckels, M. Meinke, A. Gülhan and W. Schröder

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507329

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Nonequilibrium and rarefied flows

Open Access

Experimental characterization of ultraviolet radiation of air in a high enthalpy plasma torch facility p. 353

C. J. Casses, P. J. Bertrand, C. M. Jacobs, M. E. Mac Donald and Ch. O. Laux

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507353

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Computational analysis of a rarefied hypersonic flow over combined gap/step geometries p. 369

P. H. M. Leite and W. F. N. Santos

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507369

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Open Access

Analytical model of translational nonequilibrium flow with internal degrees of freedom p. 395

I. I. Lipatov, M. M. Kuznetsov and L. V. Smotrova

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507395

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Open Access

A blunted cone in a supersonic high-enthalpy nonequilibrium air flow p. 401

V. I. Sakharov, V. V. Shtapov, E. B. Vasilevskiy and B. E. Zhestkov

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507401

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Shock waves

Open Access

Influence of leading edge bluntness on hypersonic flow in a generic internal-compression inlet p. 419

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

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507419

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A new configuration of irregular reflection of shock waves p. 437

L. G. Gvozdeva and S. A. Gavrenkov

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507437

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Conical flows near V-shaped wings with shock waves attached on leading edges p. 453

F. A. Maximov, N. A. Ostapenko and M. A. Zubin

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507453

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Wave drag reduction due to a self-aligning aerodisk p. 475

Ch. Schnepf, O. Wysocki and E. Schülein

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507475

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Stability and transition

Open Access

Prediction of laminar-turbulent transition on an airfoil at high level of free-stream turbulence p. 491

V. Chernoray

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507491

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Open Access

On the relative “receptivity” of twoand three-dimensional supersonic boundary layers to stationary disturbances at mach 2 p. 509

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

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507509

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Open Access

On modeling of laminar-turbulent transition in supersonic flows with engineering correlations and Reynolds-averaged Navier-Stokes equations p. 525

R. V. Kovalev, V. V. Kudryavtsev and D. A. Churakov

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507525

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Open Access

Effect of the local wall cooling/heating on the hypersonic boundary layer stability and transition p. 549

A. Sidorenko, Yu. Gromyko, D. Bountin, P. Polivanov and A. Maslov

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507549

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Open Access

Stability of high-speed boundary layer on a sharp cone with localized wall heating or cooling p. 569

V. G. Soudakov, A. V. Fedorov and I. V. Egorov

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507569

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Open Access

Experimental methods of the study of vortex structures excited by point injection at the leading edge of the oblique wing p. 585

S. N. Tolkachev, V. N. Gorev, G. M. Zharkova and V. N. Kovrizhina

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507585

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Open Access

Transitional flow structure on classic and wavy wings at low Reynolds numbers p. 605

I. Zverkov, V. Kozlov and A. Kryukov

Published online: 08 June 2015

DOI: https://doi.org/10.1051/eucass/201507605

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