TsAGI Science Journal
Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
Volume 43, 2012 Numéro 1
DOI: 10.1615/TsAGISciJ.v43.i1
NUMERICAL SIMULATION OF MACH NUMBER AND ANGLE OF ATTACK INFLUENCE ON REGIMES OF TRANSONIC TURBULENT FLOWS OVER AIRFOILS
pp. 1-36
DOI: 10.1615/TsAGISciJ.2012005226
GAS-DYNAMIC FEATURES OF THE FLOW FIELD OVER A MODEL OF AN INTEGRATED HYPERSONIC FLYING VEHICLE
pp. 37-58
DOI: 10.1615/TsAGISciJ.2012005188
EFFECT OF HEAT TRANSFER ON THE BEARING PROPERTIES OF A FINITE SPAN WING AT SUBSONIC SPEEDS
pp. 59-78
DOI: 10.1615/TsAGISciJ.2012005272
ON THE EXISTENCE OF THE FIRST INTEGRAL IN THE PROBLEM OF TURBULENT BOUNDARY LAYER OPTIMAL CONTROL IN SUPERSONIC FLOW
pp. 79-86
DOI: 10.1615/TsAGISciJ.2012005278
ALGORITHM FOR GENERATING SWEPT VOLUME MESHES NEAR AN AIRCRAFT WING
pp. 87-100
DOI: 10.1615/TsAGISciJ.2012005305
ABOUT THE POSSIBILITIES OF EQUIVALENT SAND-GRAIN ROUGHNESS CALCULATION FOR FLOWS IN PIPES AND IN BOUNDARY LAYERS
pp. 101-110
DOI: 10.1615/TsAGISciJ.2012005264
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