TsAGI Science Journal
Erscheint 6 Ausgaben pro Jahr
ISSN Druckformat: 1948-2590
ISSN Online: 1948-2604
Volumen 45, 2014 Ausgabe 3-4
DOI: 10.1615/TsAGISciJ.v45.i3-4
TO THE 100TH BIRTHDAY OF VLADIMIR VASILIEVICH STRUMINSKII
pp. 179-180
DOI: 10.1615/TsAGISciJ.2014011674
EXAMPLES OF NUMERICAL SIMULATION OF COMPLEX TURBULENT FLOWS AND ACCOMPANYING PROBLEMS
pp. 183-213
DOI: 10.1615/TsAGISciJ.2014011734
HIGH-RESOLUTION RANS/ILES METHOD FOR COMPLEX TURBULENT JETS
pp. 215-236
DOI: 10.1615/TsAGISciJ.2014011703
CALCULATION METHOD FOR UNSTEADY AERODYNAMIC BLADE ROW INTERACTION IN A MULTISTAGE TURBOMACHINE
pp. 255-271
DOI: 10.1615/TsAGISciJ.2014011921
SIMULATION OF PERIODIC VORTICAL STRUCTURES IN THE AIRFOIL WAKE
pp. 273-292
DOI: 10.1615/TsAGISciJ.2014011965
DEVELOPMENT OF A METHODOLOGY FOR PROPELLER NOISE CALCULATION ON HIGH-PERFORMANCE COMPUTER
pp. 293-327
DOI: 10.1615/TsAGISciJ.2014011857
EFFECT OF VORTEX GENERATORS ON THE DIRECTION DIAGRAM OF ACOUSTIC EMISSION OF SUPERSONIC JETS
pp. 329-343
DOI: 10.1615/TsAGISciJ.2014011693
STUDY OF THE DURABILITY OF ISOTROPIC PLATES UNDER WIDEBAND ACOUSTIC LOADING WITH DIFFERENT TYPES OF SPATIAL CORRELATION FUNCTIONS
pp. 345-365
DOI: 10.1615/TsAGISciJ.2014011769
COMPLEX OF ALGORITHMS AND PROGRAMS FOR CALCULATION OF AIRCRAFT NOISE
pp. 367-388
DOI: 10.1615/TsAGISciJ.2014011838
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