TsAGI Science Journal
Выходит 6 номеров в год
ISSN Печать: 1948-2590
ISSN Онлайн: 1948-2604
Том 48, 2017 Выпуск 6
DOI: 10.1615/TsAGISciJ.v48.i6
SELF-SIMILAR SOLUTIONS OF THE JEFFERY–HAMEL TYPE FOR COMPRESSIBLE VISCOUS GAS FLOW
pp. 505-514
DOI: 10.1615/TsAGISciJ.2018025813
SIMULATION OF THE FLOW IN AIRCRAFT COMPLEX PNEUMATIC LINES
pp. 515-533
DOI: 10.1615/TsAGISciJ.2018025533
INVESTIGATIONS OF VOLUME-CENTERED DISCHARGE IN AIR SUPERSONIC FLOW WITH ADDITIONAL PROPANE AND OXYGEN INJECTION
pp. 535-549
DOI: 10.1615/TsAGISciJ.2018025534
COMPARISON OF FLIGHT PATH OPTIMIZATION PROBLEM SOLUTIONS BY DIRECT AND INDIRECT METHODS FOR A GUIDED AIRCRAFT MISSILE WITH A ROCKET ENGINE
pp. 551-563
DOI: 10.1615/TsAGISciJ.2018025535
APPLICATION OF THE POLYNOMIAL RITZ METHOD FOR ANALYZING DYNAMIC AEROELASTICITY CHARACTERISTICS BY TAKING INTO ACCOUNT GYROSCOPIC FORCES
pp. 565-577
DOI: 10.1615/TsAGISciJ.2018025714
NUMERICAL METHODS FOR DETERMINING TORSIONAL STIFFNESS OF PRISMATIC RODS
pp. 579-595
DOI: 10.1615/TsAGISciJ.2018025651
Последний выпуск
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