TsAGI Science Journal
Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
Volume 50, 2019 Numéro 1
DOI: 10.1615/TsAGISciJ.v50.i1
ALEKSANDR ALEKSANDROVICH NIKOLSKII: MARKING THE 100TH ANNIVERSARY OF HIS BIRTH
pp. v-vii
DOI: 10.1615/TsAGISciJ.2019030108
ANALYTICAL MODEL OF EJECTOR-TYPE ACTUATOR OPERATING UNDER STEADY AND PULSE CONDITIONS
pp. 1-14
DOI: 10.1615/TsAGISciJ.2019030080
EFFECT OF THE HORIZONTAL CANARD OF THE SHARP-EDGED FOREBODY OF THE MANEUVERABLE AIRCRAFT MODEL ON THE VORTEX FLOW STRUCTURE
pp. 15-23
DOI: 10.1615/TsAGISciJ.2019030087
NUMERICAL INVESTIGATION OF SEPARATED INCOMPRESSIBLE FLUID FLOW PAST A CIRCULAR CYLINDER WITH A SPLITTER PLATE
pp. 25-37
DOI: 10.1615/TsAGISciJ.2019030118
EXPERIMENTAL INVESTIGATION OF BOUNDARY LAYER STATE ON THE SURFACE OF HIGH-SPEED TEST VEHICLE MODEL
pp. 39-52
DOI: 10.1615/TsAGISciJ.2019030132
DETERMINATION OF THE ACOUSTIC EFFICIENCY OF MATERIALS AND STRUCTURES IN LABORATORY AND REAL CONDITIONS. PART 2: VIBRATION ABSORPTION
pp. 53-69
DOI: 10.1615/TsAGISciJ.2019030190
NUMERICAL INVESTIGATION OF ELLIPTICAL MIXED EXPANSION NOZZLE PERFORMANCE IN SUPERSONIC FLOW
pp. 71-89
DOI: 10.1615/TsAGISciJ.2019030084
INVESTIGATIONS OF FLOW PARAMETERS IN MODELS OF PRECOMBUSTION DIFFUSERS WITH SECTIONED DUCTS
pp. 91-101
DOI: 10.1615/TsAGISciJ.2019030117
PHYSICAL MODEL VIBRATION MODELING USING ARTIFICIAL FLOW
pp. 103-113
DOI: 10.1615/TsAGISciJ.2019030091
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