TsAGI Science Journal
Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
Volume 46, 2015 Numéro 5
DOI: 10.1615/TsAGISciJ.v46.i5
SELECTION OF THE RATIONAL POSITION OF A SLOTTED NOZZLE ON THE AIRFOIL WITH A SYSTEM OF TANGENTIAL JET BLOWING FOR SHOCK-INDUCED SEPARATION SUPPRESSION
pp. 411-422
DOI: 10.1615/TsAGISciJ.v46.i5.10
HIGH-TEMPERATURE CARBON DIOXIDE FLOW OVER A LONGITUDINAL CYLINDER
pp. 423-438
DOI: 10.1615/TsAGISciJ.v46.i5.20
OPTIMAL DESIGN OF THE NACELLE ASSEMBLY UNDER THE WING OF AN AIRLINER BASED ON RANS NUMERICAL SIMULATIONS
pp. 439-464
DOI: 10.1615/TsAGISciJ.v46.i5.30
THERMODYNAMIC ANALYSIS OF DUAL-MODE SCRAMJET COMBUSTOR OPERATION
pp. 465-483
DOI: 10.1615/TsAGISciJ.v46.i5.40
ABOUT THE EVALUATION OF FATIGUE CHARACTERISTICS IN THE EARLY DESIGN STAGES OF AIRCRAFT
pp. 491-507
DOI: 10.1615/TsAGISciJ.v46.i5.60
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