ICMAR-2014
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Section Number ID
0Struminsky A.B. Why Mechanics but not Quantum Mechanics? (First steps of Vladimir Struminsky in Science)
Invited paper
1Àlexeev M.M., Samsonov E.V., Lashmanova E.A., Nenahova N.A. Thermal imaging study of nonisothermal flow of transparent liquid or gas 1186
2Andreev V.N., Kozlovskii V.A., Lagutin V.I. Tubular type strain-gauge balance for jet models wind tunnel tests 2280
3Baev V.K. Energy transformation at external burning 394
4Baev V.K., Chusov D.V. Heat exchange of cylinder in rectangular cavity streamlined by counter flows393
5Baev V.K., Frolov A.D. Thermal and physical characteristics of porous NiAl SHS-materials497
6Bayanov R.I. Numerical model of a two-phase stream around the cylinder with a phase transition3211
7Bazhaykin A.N., Baev V.K. Burning in countermoving jets396
8Borodulin V.I., Ivanov A.V., Kachanov Y.S. Experimental approach to investigation of excitation of instability modes in a swept-wing boundary layer at scattering of freestream vortices on surface nonuniformities2256
9Borodulin V.I., Ivanov A.V., Kachanov Y.S., Mischenko D.A., Fedenkova A.A. Distributed excitation of 3D TollmienSchlichting waves in a boundary layer with adverse pressure gradient by freestream vortices in presence of surface nonuniformities2240
10Borodulin V.I., Ivanov A.V., Kachanov Y.S., Mischenko D.A. Experimental investigation of characteristics of steady and unsteady crossflow-instability modes developing in a 35-degree swept-airfoil boundary layer2254
11Borodulin V.I., Kachanov Y.S. Reproducibility of instantaneous and statistical characteristics of the deterministic wall turbulence2121
12Borodulin V.I., Ivanov A.V., Kachanov Y.S., Crouch J.D., Ng L.L. Criteria of swept-wing boundary-layer transition and variable N-factor methods of transition prediction2106
13Borovoy V.Ya., Egorov I.V., Mosharov V.E., Radchenko V.N., Skuratov A.S., Struminskaya I.V. Shock waves/turbulent boundary layer interference near a fin and a pair of fins at the presence of entropy layer266
14Bosnyakov I.S., Soudakov G.G. Decay mechanisms in far vortex wake behind the plane252
15Bountin D.A., Gromyko Yu.V., Kovalev R.V., Kudryavtsev V.V., Kusov A.L., Rudin N.F., Sidorenko A.A. Experimental investigations of local heating/cooling effect on laminar-turbulent boundary layer transition over 7-half angle cone model in U-6 hypersonic wind tunnel2140
16Bui V.T., Lapygin V.I. Numerical simulation of a flow around a model in test section of low-speed wind tunnel 182
17Chang P.H., Chung K.M., Chang K.C., Li K.F. Experimental study on compressible convex-corner flows319
18Dikalyuk A.S., Surzhikov S.T. Nonequilibrium spectral radiation behind the shock waves in Martian and Earth atmospheres388
19Fang J., Yao Y., Lu L., Zheltovodov A.ADirect numerical simulation of supersonic turbulent flow in an expansion-compression corner at Mach = 2.92173
20Fang J., Yao Y., Zheltovodov A.A., Lu L. Numerical simulations of two-dimensional and three-dimensional shock wave/turbulent boundary layer interactions213
21Gaifullin A.M., Kiselev N.N., Kornyakov A.A. Flow stability near a plate with a surface moving against an incoming stream248
22Garkusha V.V., Gilyov V.M., Mishnev A.S., Shpak S.I., Yakovlev V.V. Structure of the distributed information and measuring complex for data acquisition of hypersonic wind tunnel based on adiabatic compression 1229
23Goldfeld M.A., Mosharov V.E., Radchenko V.N., Starov A.V., Timofeev K.Yu. Problems of investigation of boundary layer transition by temperature sensitive paint in impulse wind tunnel IT-3021191
24Gounko Yu.P. Actual aerogasdynamic problems of high supersonic inlets3288
25Gounko Yu.P. Gasdynamic design of air-intake with nose body of star-shaped cross section and with sequential internal convergent flow compression 350
26Gounko Yu.P., Kavun I.N. Numerical simulation off-design flows over a supersonic three-dimensional air-intake 51451
27Grigoryev Yu.N., Gorobchuk A.G. Numerical modeling of plasma-chemical etching technology in CF4/H2 gas mixture441
28Gubaidullin A.A., Yakovenko A.V. Numerical investigation of the vibrating gas-filled cavity with isothermal and adiabatic boundary conditions4217
29Hanifi A., Hein S., Romano D.G., Minervino M., W?rz W., Borodulin V.I., IvanovA.V., Kachanov Y.S. Numerical and experimental realization of an infinite-swept-wing boundary-layer flow in a wind tunnel289
30Ivanov A.V., Kachanov Y.S., Mischenko D.A. Excitation of G?rtler-instability modes in concave-wall boundary layer by longitudinal freestream vortices2238
31Kartaev E.V., Lukashov V.P., Vashenko S.P., Aulchenko S.M., Kovalev O.B., Emelkin V.A., Sergachev D.V. Plasmachemical synthesis of ultrafine titania powder by the chloride method428
32Kolesnikov A.F., Gordeev A.N., Vasilevskii S.A. Study of heat transfer and predicting surface catalycity for metals and quartz for exomars entry conditions1269
33Kolosov G.L., Kosinov A.D., Yermolaev Yu.G., Semionov N.V. On nonlinear interaction of controlled disturbances in 3D supersonic boundary layer2167
34Kosinov A.D., Yermolaev Yu.G., Kolosov G.L., Panina A.V., Semionov N.V. On the effect of the incident Mach wave on the pulsation level in boundary layer of the plane delta wing2283
35Krause M., Gaisbauer U., Kr?mer E., Yermolaev Y., Kosinov A.D. Static calibration of wedge hot-film probe and determination of sensitivities for modal analysis in T-325 supersonic wind tunnel1209
36Lapygin V.I., Gorshkov A.B., Fofonov D.M., Sazonova T.V., Mikhalin V.A. Construction of configuration for a body with high lift-drag ratio minimizing the heat flux to its side surface3109
37Leu T.S., Lee C.Y. Effects of surface modification on the performance of oscillating heat pipes3110
38Lipatov I.I., Tugazakov R.J. Transverse patterns in detached spatial gas flow and associated oscillations249
39Litvinenko M.V. Influence of initial conditions (including curved channel) on the flow structure in jets2192
40Lokotko A.V. Realization of ""doubling"" methods in aerodynamic experiment for a model with duct"1219
41Lukashevich S.V., Morozov S.O., Shiplyuk A.N. Experimental investigation of the effect of ultrasonically absorptive coating on disturbances in hypersonic boundary layer of a sharp cone at the angle of attack2159
42Mazhul I.I., Gounko Yu.P. Numerical study of supersonic flows over adjacent wedges of different sweepness 359
43Palkin E., Mullyadzhanov R., Hanjalic K. URANS and LES of a flow over a cylinder at Re = 39003221
44Polivanov P.A., Sidorenko A.A., Maslov A.A. Transition effect on shock wave / boundary layer interaction at M = 1.472149
45Prikhodko Yu.M., Chekhov V.P., Fomichev V.P. Experimental research of heat-exchange characteristics of the diametrical disk FAN137
46Sander T., Altenh?fer Ph., Mundt C. Temperature measurements in a shock tube using laser-induced thermal grating spectroscopy 158
47Saren V.E. Aerogasdynamics of axial turbomañhine flowpath321
48Savelyev A.A., Zlenko N.A., Mikhaylov S.V. Shape optimization of the engine nacelle using RANS 384
49Semionov N.V., Kosinov A.D., Yermolaev Yu.G., Dryasov A.D. Experimental study of receptivity of supersonic boundary layer on swept wing at Mach number 2.52134
50Shalaev V.I. V.V. Struminsky and 3D boundary layer theory development268
51Shapeev V.P., Vorozhtsov E.V. Application of the method of collocations and least residuals for numerical solution of three-dimensional Navier Stokes equations3171
52Skomorohov S.I., Slitinskaya A.Yu., Cherny K.I. Study of flow peculiarities and vortex wake structure behind swept wings of moderate aspect ratio at subsonic speeds 363
53Soudakov V.G., Egorov I.V., Fedorov A.V. Numerical study of laminar-turbulent transition on a sharp cone with local heating or cooling291
54Stolyarov E.P. Effects of transient processes in thermal measurements with thin-film sensors171
55Tropin D.A., Fedorov A.V. Ignition delay times in the methane-air mixture in presence of iron particles4141
56Troshin A.I. Application and modification of a Reynolds stress model in problems of jets outflow1206
57Vaganov A.V., Neyland V.Ya., Noev A.Yu., Skuratov A.S., KashinV.M., Lifits A.L., Nemykin V.M. Laminar-turbulent transition on body of revolution with surface breaks267
58Volkov V.F., Mazhul I.I., Zvegintsev V.I. Features of aerodynamics of the axisymmetric model with large aspect ratio at angles of attack 3133
59Volkov V.F., Mazhul I.I., Zvegintsev V.I. Numerical estimations of sweep pylon influence on aerodynamic characteristics of the model tested in supersonic wind tunnel1135
60Yakovenko S.N. Density drop effects in evolution of the two-fluid interface256
61Yakovenko S.N., Thomas T.G., Castro I.P. Instability development scenarios in breaking gravity waves255
62Yang G., Fang J., Lu L. POD analysis of shock wave/turbulent boundary layer interaction2195
63Yatskikh A.A., Yermolaev Yu.G., Kosinov A.D., Semionov N.V. Method of the excitation of single wave packet in supersonic boundary layer222
64Yermolaev Yu.G., Yatskikh A.A., Kosinov A.D., Semionov N.V. Evolution of the pulsed wave packet in a supersonic boundary layer2147
65Zhao H., Yi M., Ni H., Liu W. Test of forced boundary-layer transition on hypersonic inlet264
66Zharkova G.Ì., Kovrizhina V.N., Petrov À.P. Panoramic liquid-crystal indicators of shear stress: three effects and three approaches to measurement1258
67Gaisbauer U., Weigand B., Yaroslavtsev M.I. Aero-thermodynamic design of a scramjet propulsion system GRK 1095 ground testing3174