TsAGI Science Journal
Published 6 issues per year
ISSN Print: 1948-2590
ISSN Online: 1948-2604
Volume 51, 2020 Issue 3
DOI: 10.1615/TsAGISciJ.v51.i3
FEATURES OF THE FLOW AROUND A MANEUVERABLE AIRPLANE OF THE TAIL-FIRST CONFIGURATION WITH TWIN VERTICAL TAILS AT HIGH ANGLES OF ATTACK
pp. 219-235
DOI: 10.1615/TsAGISciJ.2020036196
NUMERICAL INVESTIGATIONS OF THE AERODYNAMIC CHARACTERISTICS FOR AN IMPROVED AIRFOIL WITH A CONTROL SURFACE
pp. 237-249
DOI: 10.1615/TsAGISciJ.2020036190
EFFECT OF SIDESLIP ANGLE CHANGES ON THE FLOW AROUND THE AIRFRAME OF THE "CHIROK" AIRCRAFT
pp. 251-259
DOI: 10.1615/TsAGISciJ.2020036012
THE STUDY OF DISTURBANCE PROPAGATION IN FLOWS WITH REVERSED STREAMLINES
pp. 261-269
DOI: 10.1615/TsAGISciJ.2020036071
THE INFLUENCE OF THE TURBOJET BYPASS RATIO ON THE AERODYNAMIC LAYOUT OF A BUSINESS BUSINESS JET WING
pp. 271-281
DOI: 10.1615/TsAGISciJ.2020035925
LAYOUT OF NOZZLES OF A DISTRIBUTED POWER PLANT IN AN AIRFRAME
pp. 283-295
DOI: 10.1615/TsAGISciJ.2020036145
PROTOTYPING THE AERO-INERTIAL SYSTEM FOR MEASURING FLIGHT AIR PARAMETERS IN THE T-105 WIND TUNNEL
pp. 297-304
DOI: 10.1615/TsAGISciJ.2020036036
STRUCTURALLY OPTIMIZED POLYMER COMPOSITE WING DESIGN. PART 2: TOW-STEERED COMPOSITE
pp. 305-315
DOI: 10.1615/TsAGISciJ.2020036204
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