TsAGI Science Journal
Erscheint 6 Ausgaben pro Jahr
ISSN Druckformat: 1948-2590
ISSN Online: 1948-2604
Volumen 40, 2009 Ausgabe 2
DOI: 10.1615/TsAGISciJ.v40.i2
NUMERICAL SIMULATION OF AERODYNAMICS OF WINGED RE-ENTRY SPACE VEHICLE
pp. 131-149
DOI: 10.1615/TsAGISciJ.v40.i2.10
OPTIMIZATION OF THE WING SHAPE IN THE WING-BODY SYSTEM AT HYPERSONIC FLOW
pp. 151-165
DOI: 10.1615/TsAGISciJ.v40.i2.20
KINEMATIC FOUNDATIONS OF THE RANQUE EFFECT MECHANISMHEAT SEPARATION OF FLUID AND GAS FLOW IN A VORTEX TUBE
pp. 167-190
DOI: 10.1615/TsAGISciJ.v40.i2.30
FINITE SYMMETRIC DISTURBANCES PROPAGATION IN A VORTEX CORD
pp. 191-205
DOI: 10.1615/TsAGISciJ.v40.i2.40
PARAMETRIC INVESTIGATIONS OF THE EFFECT OF ICING ON THE AERODYNAMIC CHARACTERISTICS OF A WING AIRFOIL
pp. 207-216
DOI: 10.1615/TsAGISciJ.v40.i2.50
EXPERIMENTAL INVESTIGATION OF AERODYNAMIC LOADS IN THE TIP SECTIONS OF A RIGID BLADE OF AN INCLINED MODEL ROTOR
pp. 217-239
DOI: 10.1615/TsAGISciJ.v40.i2.60
DEVELOPMENT OF A MEASURING TECHNIQUE FOR THE LOW-WAVENUMBER COMPONENTS OF THE WAVENUMBER-FREQUENCY SPECTRUM OF TURBULENT WALL PRESSURE FLUCTUATIONS
pp. 241-253
DOI: 10.1615/TsAGISciJ.v40.i2.70
INVESTIGATION OF THE FLOW PATTERN NEAR THE PROPELLER IN THE SHAPED RING AND WITHOUT IT AT THRUST REVERSAL
pp. 255-263
DOI: 10.1615/TsAGISciJ.v40.i2.80
THE PRINCIPAL REGULARITIES IN ELASTIC SYSTEM VIBRATIONS AT NONUNIFORM AEROACOUSTIC EXCITATION
pp. 265-278
DOI: 10.1615/TsAGISciJ.v40.i2.90
Neueste Ausgabe
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