TsAGI Science Journal
Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
Volume 45, 2014 Numéro 8
DOI: 10.1615/TsAGISciJ.v45.i8
GRID INFLUENCE ON AIR FLOW NON-UNIFORMITY IN WIND TUNNELS
pp. 669-696
DOI: 10.1615/TsAGISciJ.2014012526
MULTIFORM PARTICLE-FLOW INTERACTION IN A CARRYING CONTINUUM GAS (REVIEW)
pp. 697-716
DOI: 10.1615/TsAGISciJ.2015013512
EXPERIMENTAL INVESTIGATION OF THE NOZZLES OF SUBSONIC AND SUPERSONIC AIRCRAFT
pp. 717-737
DOI: 10.1615/TsAGISciJ.2015013398
MODEL PRESENTATION OF THE COHERENT STRUCTURE IN THE DEVELOPED TURBULENT BOUNDARY LAYER
pp. 739-758
DOI: 10.1615/TsAGISciJ.2015013391
FLOW IN THE VICINITY OF THE PLANE OF SYMMETRY OF A DELTA WING WITH A SMALL SWEEP ANGLE IN THE STRONG INTERACTION REGIME
pp. 759-779
DOI: 10.1615/TsAGISciJ.2015013395
INVESTIGATION OF THERMOCHEMICAL STABILITY OF THERMAL PROTECTION MATERIALS
pp. 781-802
DOI: 10.1615/TsAGISciJ.2015013546
METHOD OF MANUFACTURING ACCURACY EVALUATION OF WIND TUNNEL MODELS BY MEASURING DATA FROM A COORDINATE-MEASURING MACHINE
pp. 803-824
DOI: 10.1615/TsAGISciJ.2015013357
ON POSSIBILITY OF CRITICAL FLIGHT REGIME STUDY IN WIND TUNNELS USING THREE-DEGREE-OF-FREEDOM GIMBALS
pp. 825-839
DOI: 10.1615/TsAGISciJ.2015013365
APPLICATION OF HYDRODYNAMIC ANALOGY FOR THE CALCULATION OF THE FLEXURAL CENTER OF PRISMATIC BARS COMPOSED OF DIFFERENT MATERIALS
pp. 841-850
DOI: 10.1615/TsAGISciJ.2015013361
LAMINAR-TURBULENT TRANSITION IN BOUNDARY LAYERS (REVIEW) PART 2: TRANSITION PREDICTION AND METHODS OF BOUNDARY-LAYER LAMINARIZATION
pp. 851-887
DOI: 10.1615/TsAGISciJ.2015013660
INVESTIGATION OF A SIMPLIFIED SCHEME OF MULTIPLE PLASMA ACTUATOR FOR BOUNDARY LAYER CONTROL
pp. 889-901
DOI: 10.1615/TsAGISciJ.2015013547
LAMINAR-TURBULENT HEAT TRANSFER ON THE SURFACE OF A HEMISPHERE IN HYPERSONIC AIR FLOW
pp. 903-913
DOI: 10.1615/TsAGISciJ.2015013556
ESTIMATION OF AERODYNAMIC CHARACTERISTICS OF AIRCRAFT IN FLIGHT IN ICING CONDITIONS
pp. 915-926
DOI: 10.1615/TsAGISciJ.2015013629
ANGULAR DISTRIBUTION OF FREE MOLECULAR GAS FLOW REFLECTED FROM A SOLID BODY SURFACE
pp. 927-948
DOI: 10.1615/TsAGISciJ.2015013559
SPHERICAL PROBE IN STEADY-STATE PLASMA IN A MAGNETIC FIELD: THE CASE OF A THICK SPACE-CHARGE LAYER
pp. 949-955
DOI: 10.1615/TsAGISciJ.2015013558
COMPUTATIONAL STUDY OF FLOW PARAMETERS IN THE REGION OF THE TAIL ROTOR LOCATION AT LOW SPEEDS OF SLIDING FLIGHT
pp. 957-975
DOI: 10.1615/TsAGISciJ.2015013619
ROBUST CONTROL DESIGN TO SUPPRESS WING ROCK MOTION OF A WIND-TUNNEL AIRCRAFT MODEL IN 3DOF GIMBALS
pp. 977-992
DOI: 10.1615/TsAGISciJ.2015013555
MEASUREMENTS OF DEFORMATION OF THE ADAPTIVE WING LEADING EDGE IN A WIND TUNNEL BY THE VIDEOGRAMMETRY METHOD
pp. 993-1006
DOI: 10.1615/TsAGISciJ.2015013557
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