TsAGI Science Journal
Publicou 6 edições por ano
ISSN Imprimir: 1948-2590
ISSN On-line: 1948-2604
Volume 44, 2013 Edição 3
DOI: 10.1615/TsAGISciJ.v44.i3
ABOUT INCREASE OF EFFICIENCY OF PLASMA MULTI-ACTUATOR SYSTEM FOR BOUNDARY LAYER CONTROL
pp. 305-326
DOI: 10.1615/TsAGISciJ.2013009688
SELECTION OF VISCOUS TERMS APPROXIMATION IN DISCONTINUOUS GALERKIN METHOD
pp. 327-354
DOI: 10.1615/TsAGISciJ.2013009684
AERODYNAMIC LOADS MEASUREMENTS ON AN AIRFOIL USING PIV SYSTEM
pp. 355-370
DOI: 10.1615/TsAGISciJ.2013009699
SOLUTION OF THE INVERSE PROBLEM FOR AN AIRFOIL WITHIN THE FRAMEWORK OF THE REYNOLDS AVERAGED NAVIER-STOKES EQUATIONS
pp. 371-385
DOI: 10.1615/TsAGISciJ.2013009695
ENGINEERING TECHNIQUE OF CORRECTING THE MAXIMAL LIFT COEFFICIENT OF MODELS FOR THE FULL-SCALE FLIGHT CONDITIONS
pp. 387-404
DOI: 10.1615/TsAGISciJ.2013010128
THE METHOD OF OPTIMAL PROFILING OF FLYING VEHICLE FUSELAGE AND NOZZLE AT THE CRUISING SUPERSONIC FLIGHT
pp. 405-417
DOI: 10.1615/TsAGISciJ.2013010195
GENERATION OF THE ALGORITHM OF SYNCHRONIZATION OF RELAY-HYSTERETIC ELEMENTS IN DIGITAL REDUNDANT CONTROL SYSTEM BY MEANS OF FINITE STATE AUTOMATION
pp. 419-432
DOI: 10.1615/TsAGISciJ.2013009686
NONCONTACT MEASUREMENTS OF NORMAL DEFORMATION FIELDS OF A CONSTRUCTION SURFACE BY VIDEOGRAMMETRY METHODS WHILE STRENGTH TESTING
pp. 433-444
DOI: 10.1615/TsAGISciJ.2013010258
Última edição
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