TsAGI Science Journal
Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
Volume 47, 2016 Numéro 2
DOI: 10.1615/TsAGISciJ.v47.i2
INVESTIGATION OF THE FLOW STRUCTURE AND ACOUSTIC FIELD OF A TURBULENT JET WITH HIGH SWIRLING INTENSITY
pp. 111-137
DOI: 10.1615/TsAGISciJ.2016017878
INVESTIGATION OF NOZZLE GEOMETRY AND OUTFLOW REGIME EFFECT ON FLOW PARAMETERS AND TURBULENT JET NOISE BY THE HIGH-RESOLUTION RANS/ILES METHOD
pp. 139-158
DOI: 10.1615/TsAGISciJ.2016017768
APPLICATION OF THE HIGH-RESOLUTION RANS/ILES TECHNOLOGY FOR FLOW SIMULATION AND THE NEARBY ACOUSTIC FIELD OF NEAR-WALL JETS AND MIXING LAYERS
pp. 159-183
DOI: 10.1615/TsAGISciJ.2016017766
EVALUATION OF THE TONE NOISE OF A FAN ON THE BASIS OF THE 3D COMPUTATION OF ROTOR−STATOR INTERACTION
pp. 185-205
DOI: 10.1615/TsAGISciJ.2016017665
INVESTIGATION OF THE EFFICIENCY OF APPLICATION OF A VIBRATION-ABSORBING MATERIAL WITH A REINFORCING LAYER FOR IMPROVING SOUND INSULATION OF STRUCTURAL ELEMENTS OF THE FUSELAGE
pp. 223-236
DOI: 10.1615/TsAGISciJ.2016017888
Dernier numéro
KIRILL IVANOVICH SYPALO−50TH ANNIVERSARY
NUMERICAL STUDY OF THE DISTURBANCES GENERATED BY MICROJETS IN A SUPERSONIC FLAT-PLATE BOUNDARY LAYER
ANALYSIS OF THE MOVING DETONATION INTERACTION WITH TURBULENT BOUNDARY LAYERS IN A DUCT ON THE BASIS OF NUMERICAL SIMULATION
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