TsAGI Science Journal
Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
Volume 45, 2014 Numéro 6
DOI: 10.1615/TsAGISciJ.v45.i6
CONGRATULATIONS TO VOLF YAKOVLEVICH BOROVOY ON HIS 90TH BIRTHDAY!
pp. 479-480
DOI: 10.1615/TsAGISciJ.2014012482
INVESTIGATION OF THE FLOW AHEAD OF THE THROAT CROSS SECTION OF AN IDEAL SONIC NOZZLE
pp. 481-494
DOI: 10.1615/TsAGISciJ.2014012231
EXPERIMENTAL INVESTIGATIONS OF RESONANT AERO-ACOUSTIC EXCITATION OF CAVITY DEPTH MODES BY A FLOW
pp. 495-508
DOI: 10.1615/TsAGISciJ.2014012209
ANALYTICAL SOLUTIONS OF SPACE FLIGHT EQUATIONS WITH LOW THRUST
pp. 509-529
DOI: 10.1615/TsAGISciJ.2014012227
ON THE POSSIBILITY OF LAMINAR FLOW CONTROL ON A SWEPT WING BY MEANS OF PLASMA ACTUATORS
pp. 531-554
DOI: 10.1615/TsAGISciJ.2014012527
EFFECT OF ICING ON THE AERODYNAMIC CHARACTERISTICS OF AIRCRAFT DURING LANDING
pp. 555-570
DOI: 10.1615/TsAGISciJ.2014012540
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