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1
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Validation of global aeropropulsive characteristics of integrated configurations
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April
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Mazhul, I.7
Yaroslavtsev, M.8
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2
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0012534195
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Study on drag-thrust forces of a scramjet model in blow-down and hot-shot wind tunnels
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Inst. of Theoretical and Applied Mechanics, Novosibirsk, Russia
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Adamov, N., Goonko, Y., Kharitonov, A., Latypov, A., Mazhul, I., Yaroslavtsev, M., Chalot, F., Rostand, P., and Perrier, P., "Study on Drag-Thrust Forces of a Scramjet Model in Blow-Down and Hot-Shot Wind Tunnels," Proceedings of the International Conference on the Methods of Aerophysical Research (ICMAR'98), Inst. of Theoretical and Applied Mechanics, Novosibirsk, Russia, 1998, Pt. 3, pp. 3-9.
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Yaroslavtsev, M.6
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Rostand, P.8
Perrier, P.9
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3
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Integration of an air-breathing hypersonic airplane
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Numerical and experimental investigation of an airframe-integrated inlet for high velocities
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Inst. of Theoretical and Applied Mechanics, Novosibirsk, Russia, in Russian
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Dem'yanenko, V. S., Grigor'ev, V. D., Kharitonov, A. M., Pisarenko, K. I., and Volonikhin, I. I., "Supersonic Wind Tunnel T-313," Aerophysical Studies, Inst. of Theoretical and Applied Mechanics, Novosibirsk, Russia, 1972, pp. 8-11 (in Russian).
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Pisarenko, K.I.4
Volonikhin, I.I.5
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12
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3643107258
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Multichannel pressure meter MID-100
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Inst. of Theoretical and Applied Mechanics, Novosibirsk, Russia, in Russian
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Amelina, M. A., Brodetsky, M. D., Kharitonov, A. M., Ol'khovikov, G. P., Volonikhin, I. I., Vyshenkov, Y. I., and Zuenko, V. S., "Multichannel Pressure Meter MID-100," Techniques and Instrumentation for Aerodynamic Experiment, Inst. of Theoretical and Applied Mechanics, Novosibirsk, Russia, 1978, pp. 98-113 (in Russian).
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Volonikhin, I.I.5
Vyshenkov, Y.I.6
Zuenko, V.S.7
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13
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85038465601
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Study on measurement errors of reduced pressure coefficients at supersonic velocities
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Inst. of Theoretical and Applied Mechanics, Novosibirsk, Russia, in Russian
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Brodetsky, M. D., Brouk, S. M., and Makhnin, A. M., "Study on Measurement Errors of Reduced Pressure Coefficients at Supersonic Velocities," Aerodynamic Studies of Non-Plane Wings, Inst. of Theoretical and Applied Mechanics, Novosibirsk, Russia, 1977, pp. 94-113 (in Russian).
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Brodetsky, M.D.1
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14
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Stabilization of gas parameters in plenum chamber of hot-shot wind tunnel
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Techniques and Instrumentation for Measurement of Gas Flows
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Petunin, A.N.1
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0012532993
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A gauge for measurement of heat flux in hypersonic wind tunnels
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Advances in Hypervelocity Techniques, edited by A. M. Krill, Plenum, New York, Mashinostroenie, Moscow, in Russian
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Ledford, R. L., "A Gauge for Measurement of Heat Flux in Hypersonic Wind Tunnels," Advances in Hypervelocity Techniques, Proceedings of the Second Symposium on Hypervelocity Techniques, edited by A. M. Krill, Plenum, New York, 1962; Mashinostroenie, Moscow, 1965, pp. 458-449 (in Russian).
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85038450903
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Errors of heat flux reconstruction by calorimetric convenors
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in Russian
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0037804429
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A technique for determination of heat fluxes and force characteristics of ramjet/scramjet models in a hot-shot wind tunnel
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Siberian. Branch, Russian Academy of Sciences, Novosibirsk, Russia
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Goonko, Y., Kharitonov, A., Latypov, A., Mazhul, I., and Yaroslavtsev, M., "A Technique for Determination of Heat Fluxes and Force Characteristics of Ramjet/Scramjet Models in a Hot-Shot Wind Tunnel," Proceedings of the International Conference on the Methods of Aerophysical Research (ICMAR'2000), Siberian. Branch, Russian Academy of Sciences, Novosibirsk, Russia, 2000, Pt. 3, pp. 51-58.
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Inst. of Theoretical and Applied Mechanics, Preprint 15-89, Novosibirsk, Russia, in Russian
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Goonko, Y. P., and Markelov, G. N., "Application of Relations for an Oblique Shock Wave in the Two-Dimensional Flow to Problems on Plane Shock Waves of General Spatial Orientation," Inst. of Theoretical and Applied Mechanics, Preprint 15-89, Novosibirsk, Russia, 1989 (in Russian).
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Application of Relations for an Oblique Shock Wave in the Two-Dimensional Flow to Problems on Plane Shock Waves of General Spatial Orientation
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Goonko, Y.P.1
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Gas-dynamic design of waveriders with convergent compression surfaces and inlets
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Goonko, Y. P., Markelov, G. N., and Shashkin, A. P., "Gas-Dynamic Design of Waveriders with Convergent Compression Surfaces and Inlets," Siberian Physical-Technical Journal, No. 4, 1993, pp. 47-55 (in Russian).
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An investigation of boundary layer transition on a wing airfoil at supersonic velocities
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Kornilov, V. I., Levchenko, V. I., and Kharitonov, A. M., "An Investigation of Boundary Layer Transition on a Wing Airfoil at Supersonic Velocities," Izvestiya SB AS USSR, Seriya Technicheskikh Nauk, No. 3, Issue 1, 1971, pp. 15-20 (in Russian).
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Effects of sweep angle and unit reynolds number on transition of boundary layer at supersonic speeds
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Kalinina, S. V., and Kornilov, V. I., "Effects of Sweep Angle and Unit Reynolds Number on Transition of Boundary Layer at Supersonic Speeds," Prikladnaya Mekhanika i Tekhnicheskaya Physika, No. 1, 1973, pp. 159-162 (in Russian).
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Experimental study on transition of laminar boundary layer to turbulent one at supersonic velocities
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Struminsky, V. V., Kharitonov, A. M., and Chernykh, V. V., "Experimental Study on Transition of Laminar Boundary Layer to Turbulent One at Supersonic Velocities," Mechanika Zhidkosti i Gasa, No. 2, 1972, pp. 30-34 (in Russian).
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Ph.D. Dissertation, Inst. of Theoretical and Applied Mechanics, Novosibirsk, Russia, in Russian
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Dem'yanenko, V. S., "Experimental Study of Three-Dimensional Supersonic Flows in Region of Interferaction Between Intersecting Plane Surfaces," Ph.D. Dissertation, Inst. of Theoretical and Applied Mechanics, Novosibirsk, Russia, 1973 (in Russian).
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Experimental Study of Three-Dimensional Supersonic Flows in Region of Interferaction Between Intersecting Plane Surfaces
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Dem'Yanenko, V.S.1
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0012593510
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Three-dimensional interaction of shock waves with turbulent bounadary layer in corner flows
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Dem'yanenko, V. S., and Igoumnov, V. A., "Three-Dimensional Interaction of Shock Waves with Turbulent Bounadary Layer in Corner Flows," Izvestiya SB AS USSR, Seriya Technicheskikh Nauk, No. 8, Issue 2, 1975, pp. 56-62 (in Russian).
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Comparison of shock-induced two- and three-dimensional incipient turbulent separation
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Theory of boundary layer
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Study on transition of boundary layer on a cone in hypersonic flow at various angles of attack
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Davlet-Kil'deev, R. Z., "Study on Transition of Boundary Layer on a Cone in Hypersonic Flow at Various Angles of Attack," Trudy TsAGI, No. 1881, 1977 (in Russian).
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Davlet-Kil'deev, R.Z.1
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Calculation of skin friction and heat transfer coefficients for laminar boundary layer on flat plate, cone, and near stagnation point of blunted bodies without dissociation
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in Russian
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Bashkin, V. A., "Calculation of Skin Friction and Heat Transfer Coefficients for Laminar Boundary Layer on Flat Plate, Cone, and Near Stagnation Point of Blunted Bodies Without Dissociation," Trudy TsAGI, No. 973, 1965 (in Russian).
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Trudy TsAGI
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Calculation of friction and heat transfer coefficients for a flat plate in the presence of heat transfer at supersonic speeds
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Kovalenko, V. M., "Calculation of Friction and Heat Transfer Coefficients for a Flat Plate in the Presence of Heat Transfer at Supersonic Speeds," Trudy TsAGI, No. 1084, 1967 (in Russian).
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Measurements of the triple shock wave/turbulent boundary-layer interaction
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Narayanswami, N., Knight, D. D., Bogdonoff, S. M., and Horstman, C. C., "Interactions Between Crossing Oblique Shocks and a Turbulent Boundary Layer," AIAA Journal, Vol. 30, No. 8, 1992, pp. 1945-1952.
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