TsAGI Science Journal
Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
Volume 44, 2013 Numéro 1
DOI: 10.1615/TsAGISciJ.v44.i1
LAMINAR−TURBULENT TRANSITION IN BOUNDARY LAYERS (REVIEW). PART. 1: MAIN TYPES OF LAMINAR−TURBULENT TRANSITION IN A SWEPT-WING BOUNDARY LAYER
pp. 1-63
DOI: 10.1615/TsAGISciJ.2013007932
NUMERICAL MODELING OF THE POSITION OF A LAMINAR-TURBULENT TRANSITION ON A WING WITH THE LAMINAR AIRFOIL LV6
pp. 65-76
DOI: 10.1615/TsAGISciJ.2013007864
EXPERIMENTAL INVESTIGATION OF DIELECTRIC BARRIER DISCHARGE EFFECT ON VELOCITY AND PRESSURE PULSATIONS IN A SUBSONIC JET
pp. 77-91
DOI: 10.1615/TsAGISciJ.2013007845
PHENOMENON OF FORMATION OF PRESSURE PULSATIONS DURING THE INCIDENCE OF THE SHOCK WAVES ON THE BOUNDARY LAYER
pp. 93-110
DOI: 10.1615/TsAGISciJ.2013007866
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF AERODYNAMIC CHARACTERISTICS OF THE HYPERSONIC AIRCRAFT MODEL OF INTEGRATED CONFIGURATION
pp. 111-127
DOI: 10.1615/TsAGISciJ.2013007838
THE POSSIBILITY OF EXCEEDING THE BETZ−JOUKOWSKY MAXIMUM EFFICIENCY OF WIND TURBINES
pp. 129-140
DOI: 10.1615/TsAGISciJ.2013007939
ANALYSIS OF DYNAMIC PROPERTIES OF AIRCRAFT WITH DATA EQUALIZATION BETWEEN REDUNDANT CHANNELS OF DIGITAL CONTROL SYSTEM
pp. 141-157
DOI: 10.1615/TsAGISciJ.2013007844
INFLUENCE OF A PERIODIC FLOW NON-UNIFORMITY ON STABILITY OF AEROELASTIC VIBRATIONS OF A WING
pp. 159-170
DOI: 10.1615/TsAGISciJ.2013007867
Dernier numéro
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