TsAGI Science Journal
Published 6 issues per year
ISSN Print: 1948-2590
ISSN Online: 1948-2604
Volume 42, 2011 Issue 3
DOI: 10.1615/TsAGISciJ.v42.i3
MODELING OF SONIC BOOM WAVE PROPAGATION THROUGH TURBULENCE
pp. 275-288
DOI: 10.1615/TsAGISciJ.v42.i3.10
EXPERIMENTAL INVESTIGATIONS OF SERIES OF NONEQUILIBRIUM ELECTRODE DISCHARGE SHEMES IN OBJECTIVES OF IGNITION AND COMBUSTION STABILIZATION IN SUPERSONIC FLOWS
pp. 289-319
DOI: 10.1615/TsAGISciJ.v42.i3.20
PROBLEM OF INTERFERENCE OF AN OGIVAL BODY OF REVOLUTION WITH THE WIND-TUNNEL STING AND SPECIFIC FEATURES OF COMPUTING THIS PROBLEM
pp. 321-344
DOI: 10.1615/TsAGISciJ.v42.i3.30
ATTENUATION OF CROSS FLOW-TYPE INSTABILITY IN A 3D BOUNDARY LAYER DUE TO VOLUMETRIC FORCE IMPACT
pp. 345-360
DOI: 10.1615/TsAGISciJ.v42.i3.40
METHOD OF CALCULATING AERODYNAMIC CHARACTERISTICS OF HYPERSONIC FLYING VEHICLE ELEMENTS WITH ALLOWANCE FOR VISCOSITY, ENTROPY EFFECTS, AND VORTEX INTERACTION
pp. 361-371
DOI: 10.1615/TsAGISciJ.v42.i3.50
NUMERICAL SIMULATION OF SUPERSONIC FLOW OVER LONG CAVITIES
pp. 373-388
DOI: 10.1615/TsAGISciJ.v42.i3.60
DEVELOPMENT OF NON-STATIONARY PERTURBATIONS IN THE BOUNDARY LAYER CAUSED BY SLOT SUCTION
pp. 389-402
DOI: 10.1615/TsAGISciJ.v42.i3.70
DEVELOPMENT OF EQUALIZING GRIDS WITH LOW DRAG COEFFICIENCTS FOR WIND TUNNELS
pp. 403-413
DOI: 10.1615/TsAGISciJ.v42.i3.80
THE PROBLEM OF MANEUVERABLE FLIGHT VEHICLE FLUTTER CONSIDERING OSCILLATIONS OF TWO PRINCIPAL PLANES
pp. 415-426
DOI: 10.1615/TsAGISciJ.v42.i3.90
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KIRILL IVANOVICH SYPALO−50TH ANNIVERSARY
NUMERICAL STUDY OF THE DISTURBANCES GENERATED BY MICROJETS IN A SUPERSONIC FLAT-PLATE BOUNDARY LAYER
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EXPERIMENTAL STUDY OF COUNTERFLOW BLOWING IN HIGH-SPEED FLOW THROUGH AN ASYMMETRIC SLOT IN THE LEADING EDGE OF A SHARP WEDGE
ASYMPTOTIC SOLUTIONS TO HYPERSONIC BOUNDARY LAYER EQUATIONS ON A FLAT WING WITH A POINT OF INFLECTION ON THE LEADING EDGE
WAVE MODEL OF ORGANIZED STRUCTURES IN A TURBULENT BOUNDARY LAYER ON A PLATE WITH ZERO LONGITUDINAL PRESSURE GRADIENT
NUMERICAL SIMULATION OF THE FLOW AROUND LANDSCAPE FRAGMENTS AND SOLUTION VERIFICATION
POLYNOMIAL REPRESENTATION OF THERMODYNAMIC PROPERTIES OF COMBINED FUEL SYSTEMS IN RAMJET SIMULATION MODELS
A MODEL TEST METHODOLOGY FOR THE INVESTIGATION OF AN ELASTICALLY SCALED MAIN ROTOR
INDEX, VOLUME 51, 2020