TsAGI Science Journal
Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
Volume 46, 2015 Numéro 2
DOI: 10.1615/TsAGISciJ.v46.i2
NUMERICAL INVESTIGATION OF A STEADY VISCOUS INCOMPRESSIBLE FLUID FLOW OVER A FAMILY OF ELLIPTIC CYLINDERS
pp. 87-105
DOI: 10.1615/TsAGISciJ.2015014062
AXISYMMETRIC BODY AT AN ANGLE OF ATTACK IN HYPERSONIC FLOW: HEAT PROBLEM
pp. 107-121
DOI: 10.1615/TsAGISciJ.2015013894
CHARACTERISTICS INVESTIGATION OF 2D AND 3D INTAKES OF SUPERSONIC PASSENGER AIRCRAFT
pp. 123-142
DOI: 10.1615/TsAGISciJ.2015013901
PARAMETRIC EXPERIMENTAL INVESTIGATIONS ON THE CROSS CORRELATION OF THE PRESSURE FLUCTUATIONS GENERATED BY A CASCADE OF "FORWARD-FACING STEP/BACKWARD-FACING STEP" COMBINATIONS
pp. 143-160
DOI: 10.1615/TsAGISciJ.2015014266
MEASUREMENTS OF DEFORMATION OF THE PASSENGER PLANE WING IN FLIGHT BY THE VIDEOGRAMMETRY METHOD
pp. 161-173
DOI: 10.1615/TsAGISciJ.2015013895
METHOD OF DETERMINATION OF RATIONAL DESIGN PARAMETERS USING THE FINITE-ELEMENT METHOD
pp. 175-192
DOI: 10.1615/TsAGISciJ.2015014219
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