TsAGI Science Journal
年間 6 号発行
ISSN 印刷: 1948-2590
ISSN オンライン: 1948-2604
巻 46, 2015 発行 3
DOI: 10.1615/TsAGISciJ.v46.i3
SELF-SIMILAR AND LIMITING SOLUTIONS OF TURBULENT BOUNDARY LAYER EQUATIONS: CONDITIONS OF D'ALEMBERT'S PARADOX
pp. 193-207
DOI: 10.1615/TsAGISciJ.2015014084
EVOLUTION OF VORTICITY IN SWIRLING AXISYMMETRIC FLOWS OF A VISCOUS INCOMPRESSIBLE FLUID
pp. 209-217
DOI: 10.1615/TsAGISciJ.2015014086
NONUNIQUENESS OF THE SOLUTION IN THE VICINITY OF THE PLANE OF SYMMETRY OF A DELTA WING IN A HYPERSONIC FLOWWITH STRONG INTERACTION
pp. 231-245
DOI: 10.1615/TsAGISciJ.2015014302
ACTIVE CANCELLATION OF THE CROSSFLOWIN A SUBSONIC BOUNDARY LAYER ON AN OBLIQUE WING
pp. 247-258
DOI: 10.1615/TsAGISciJ.2015014303
DESIGN OF FLY-BY-WIRE CONTROL SYSTEM ALGORITHMS FOR ADVANCED HIGH-SPEED HELICOPTER
pp. 259-287
DOI: 10.1615/TsAGISciJ.2015014083
SOME ASPECTS OF MODELING A HIGH-ASPECT-RATIO COMPOSITE WING-BOX BY AN ANISOTROPIC BEAM
pp. 289-305
DOI: 10.1615/TsAGISciJ.2015014306
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