TsAGI Science Journal
Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
Volume 46, 2015 Numéro 6
DOI: 10.1615/TsAGISciJ.v46.i6
NEW METHOD OF OPTICAL INVESTIGATIONS OF BOUNDARY LAYER STATE IN AERODYNAMIC EXPERIMENT
pp. 509-517
DOI: 10.1615/TsAGISciJ.v46.i6.10
METHOD OF OPTIMAL AERODYNAMIC DESIGN OF THE NACELLE FOR THE MAIN PROPULSION SYSTEM WITH A HIGH BYPASS RATIO
pp. 533-558
DOI: 10.1615/TsAGISciJ.v46.i6.30
NUMERICAL ANALYSIS OF SINGLE-EXPANSION RAMP NOZZLE PERFORMANCE IN SUPERSONIC FLOW
pp. 559-576
DOI: 10.1615/TsAGISciJ.v46.i6.40
METHOD OF COMPUTATIONS OF LOADS AT THE DESIGN OF ROTOR UNITS AND HELICOPTER CONTROL SYSTEM
pp. 577-590
DOI: 10.1615/TsAGISciJ.v46.i6.50
THE STATIC PRESSURE INFLUENCE ON ELECTROPHYSICAL CHARACTERISTICS OF A DIELECTRIC BARRIER DISCHARGE
pp. 591-607
DOI: 10.1615/TsAGISciJ.v46.i6.60
HYDROGEN INJECTION INTO A SUPERSONIC FLOWOF AIR IN A CHANNEL WITH RADIAL PYLONS
pp. 609-618
DOI: 10.1615/TsAGISciJ.v46.i6.70
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