TsAGI Science Journal
Выходит 6 номеров в год
ISSN Печать: 1948-2590
ISSN Онлайн: 1948-2604
Том 40, 2009 Выпуск 3
DOI: 10.1615/TsAGISciJ.v40.i3
DEVELOPMENT OF AEROSHAPE AND INVESTIGATION OF SMALL-SIZED WINGED RE-ENTRY VEHICLE AEROTHERMODYNAMIC CHARACTERISTICS
pp. 279-298
DOI: 10.1615/TsAGISciJ.v40.i3.10
EXPERIMENTAL AND NUMERICAL INVESTIGATIONS OF BOUNDARY LAYER TRANSITION ON BLUNTED CONES AT SUPERSONIC FLOW
pp. 309-319
DOI: 10.1615/TsAGISciJ.v40.i3.30
COMPUTATIONAL ANALYSIS OF THE EFFICIENCY OF A PROPELLER IN A VISCOUS WAKE USING NAVIER-STOKES EQUATIONS
pp. 321-331
DOI: 10.1615/TsAGISciJ.v40.i3.40
METHOD FOR DETERMINATION OF AXIAL COMPRESSOR PARAMETERS AT THE BASIC POINTS OF STALLING BRANCH CHARACTERISTICS
pp. 333-353
DOI: 10.1615/TsAGISciJ.v40.i3.50
VIBRATIONS AND ACOUSTIC RADIATION OF THIN-WALLED STRUCTURES AT NONUNIFORM AEROACOUSTIC EXCITATION
pp. 367-378
DOI: 10.1615/TsAGISciJ.v40.i3.70
ROPE SYSTEM PARAMETRIC CONFIGURATION FOR AIRCRAFT TOWING WITH GUARANTEED VERTICAL SHIFT RANGE
pp. 379-391
DOI: 10.1615/TsAGISciJ.v40.i3.80
Последний выпуск
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