俄罗斯空气动力研究所中心学报
每年出版 6 期
ISSN 打印: 1948-2590
ISSN 在线: 1948-2604
卷 50, 2019 册 4
DOI: 10.1615/TsAGISciJ.v50.i4
ON SMALL DISTURBANCES OF A BOUNDARY LAYER WITHIN A REVERSE FLOW REGION
pp. 361-374
DOI: 10.1615/TsAGISciJ.2019031648
DESIGNING A WING AIRFOIL BASED ON AN ANALYTICAL REPRESENTATION OF THE CONTOUR AND NUMERICAL SOLUTIONS OF THE NAVIER-STOKES EQUATIONS
pp. 375-386
DOI: 10.1615/TsAGISciJ.2019031622
TO AIRCRAFT TRAJECTORY OPTIMIZATION IN THE REAL ATMOSPHERE
pp. 387-410
DOI: 10.1615/TsAGISciJ.2019031677
ASSESSMENT OF STATIC LOAD STRENGTH OF LAMINATED COMPOSITES
pp. 411-427
DOI: 10.1615/TsAGISciJ.2019031669
INVESTIGATION OF CALCULATION ERROR FOR STRESS INTENSITY FACTORS APPLYING THE J-INTEGRAL METHOD
pp. 429-442
DOI: 10.1615/TsAGISciJ.2019031630
ANALYSIS OF THE BEHAVIOR OF COMPRESSED LATTICE COMPOSITE RIBS WITH INITIAL DELAMINATION
pp. 443-452
DOI: 10.1615/TsAGISciJ.2019031636
PROBABILISTIC APPROACH TO DETERMINING THE RESERVE FACTOR OF A HELICOPTER STRUCTURE AT VARIOUS LIFE CYCLE STAGES
pp. 453-459
DOI: 10.1615/TsAGISciJ.2019031659
最新一期
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