TsAGI Science Journal
年間 6 号発行
ISSN 印刷: 1948-2590
ISSN オンライン: 1948-2604
巻 42, 2011 発行 1
DOI: 10.1615/TsAGISciJ.v42.i1
EXPERIMENTAL INVESTIGATION OF THE SUPERSONIC BOUNDARY LAYER STABILITY ON A SWEPT WING AT MACH NUMBER M = 2
pp. 1-12
DOI: 10.1615/TsAGISciJ.v42.i1.10
CIRCULAR CYLINDER IN THE TRANSONIC FLOWOF A VISCOUS PERFECT GAS
pp. 13-36
DOI: 10.1615/TsAGISciJ.v42.i1.20
FEATURES OF NUMERICAL MODELING OF A DIELECTRIC BARRIER DISCHARGE
pp. 47-69
DOI: 10.1615/TsAGISciJ.v42.i1.40
FACILITY FOR INVESTIGATIONS OF TOTAL HEMISPHERICAL EMISSIVITY OF HEAT PROTECTION MATERIALS AND THERMAL CONTROL COATINGS
pp. 71-82
DOI: 10.1615/TsAGISciJ.v42.i1.50
DESCRIPTION OF MARKOVIAN PROCESS DYNAMICS IN AN EXTENDED SPACE OF VARIABLES
pp. 83-108
DOI: 10.1615/TsAGISciJ.v42.i1.60
SYNTHESIS OF A SYNCHRONIZATION ALGORITHM FOR INTEGRATORS OF A DIGITAL REDUNDANT CONTROL SYSTEM
pp. 109-118
DOI: 10.1615/TsAGISciJ.v42.i1.70
APPLICATION OF THE MODEL OF VARIABLE DENSITY AT EARLY STAGES OF WING DESIGN
pp. 119-133
DOI: 10.1615/TsAGISciJ.v42.i1.80
最新号
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