TsAGI Science Journal
Published 6 issues per year
ISSN Print: 1948-2590
ISSN Online: 1948-2604
Volume 42, 2011 Issue 2
DOI: 10.1615/TsAGISciJ.v42.i2
FOR THE 100th ANNIVERSARY OF THE MSTISLAV V. KELDYSH'S BIRTH. THE BEGINNING OF CREATIVE WAYS: WORK AT TSAGI
pp. 135-140
DOI: 10.1615/TsAGISciJ.v42.i2.10
ASYMPTOTIC SOLUTION OF THE PROBLEM OF A SUBSONIC GAS FLOW AROUND AN AIRFOIL WITH A LOCAL SUPERSONIC AREA FORMATION
pp. 141-149
DOI: 10.1615/TsAGISciJ.v42.i2.20
FLOW IN THE NEIGHBORHOOD OF THE BREAKPOINT OF THE LEADING EDGE THIN WING AT THE STRONG INTERACTION REGIME
pp. 151-167
DOI: 10.1615/TsAGISciJ.v42.i2.30
PECULIARITIES OF DRAG OF THE REVOLUTION POWER-LAW BODIES
pp. 169-177
DOI: 10.1615/TsAGISciJ.v42.i2.40
AERODYNAMIC CALCULATION METHOD OF THE MAIN ROTOR TAKING INTO ACCOUNT DIFFUSION OF FREE VORTICES FOR SMALL FLIGHT SPEEDS
pp. 179-203
DOI: 10.1615/TsAGISciJ.v42.i2.50
FLOW AROUND A SOLID BODY OF THE HEATED SUPERSONIC GAS-DISPERSED JET WITH ACCOUNT OF THE ROTATION OF THE REJECTED PARTICLES
pp. 205-225
DOI: 10.1615/TsAGISciJ.v42.i2.60
MODELING OF DIELECTRIC BARRIER DISCHARGE ACTUATORS AT VARIOUS GAS PRESSURES AND ESTIMATION OF THEIR INFLUENCE ON SHEAR FLOWS
pp. 227-243
DOI: 10.1615/TsAGISciJ.v42.i2.70
STABILITY EVALUATION OF AN AIRPLANE WITH A DIGITAL MULTIRATE CONTROL SYSTEM IN A LATERAL MOTION
pp. 245-258
DOI: 10.1615/TsAGISciJ.v42.i2.80
Latest Issue
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