TsAGI Science Journal
Erscheint 6 Ausgaben pro Jahr
ISSN Druckformat: 1948-2590
ISSN Online: 1948-2604
Volumen 49, 2018 Ausgabe 6
DOI: 10.1615/TsAGISciJ.v49.i6
INTERACTION OF SHOCK WAVES NEAR A CYLINDER PERPENDICULAR TO A BLUNT PLATE, PART II: HEAT TRANSFER ON A CYLINDER
pp. 581-594
DOI: 10.1615/TsAGISciJ.2018029217
EXPERIMENTAL INVESTIGATION OF BOUNDARY LAYER STATE ON THE MODEL OF INTEGRATED DESIGN HIGH-SPEED VEHICLE AND ITS IMPACT UPON THE CONVERGENT INTAKE STARTING
pp. 595-609
DOI: 10.1615/TsAGISciJ.2018029191
METHOD OF COMPUTATION OF AERODYNAMIC CHARACTERISTICS OF THE WING–TAIL CONFIGURATION IN TRANSONIC CRUISE FLIGHT
pp. 611-618
DOI: 10.1615/TsAGISciJ.2018029236
HYPERSONIC WIND TUNNELS BASED ON PRESSURE MULTIPLIERS, PART II: CAPABILITIES OF HYPERSONIC WIND TUNNELS BASED ON VARIOUS SCHEMES
pp. 625-643
DOI: 10.1615/TsAGISciJ.2018029457
EFFECT OF THE POROSITY PARAMETER OF PERFORATED WALLS ON THE AMPLITUDE OF THE REFLECTED DISTURBANCE IN THE VICINITY OF A MODEL FOR SUPERSONIC FLOWS
pp. 645-651
DOI: 10.1615/TsAGISciJ.2018029193
THE EFFECT OF CYCLIC LOADING ON THE RESIDUAL STRESSES AND STRESS INTENSITY FACTORS
pp. 653-674
DOI: 10.1615/TsAGISciJ.2018029442
THE INVERSE PROBLEM OF DETERMINING THE TEMPERATURE DEPENDENCE OF HEMISPHERICAL TOTAL EMISSIVITY
pp. 675-682
DOI: 10.1615/TsAGISciJ.2018028773
Neueste Ausgabe
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