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 47, 2016 册 7
DOI: 10.1615/TsAGISciJ.v47.i7
PASSIVE CONTROL OF OBLIQUE-SHOCK INTERACTION WITH THE TURBULENT BOUNDARY LAYER
pp. 665-683
DOI: 10.1615/TsAGISciJ.2017019835
ANALYSIS OF SUBSONIC VORTEX FLOW OVER THE MODEL OF MANEUVERABLE AIRCRAFT USING COMPUTATIONAL FLUID DYNAMICS METHODS
pp. 685-707
DOI: 10.1615/TsAGISciJ.2017019838
PROSPECTS OF CREATION OF NEXT-GENERATION REGENERATIVE GAS HEATERS USED IN INDUSTRIAL WIND TUNNELS FOR RESEARCH AT HIGH REYNOLDS NUMBERS
pp. 709-731
DOI: 10.1615/TsAGISciJ.2017019742
EXPERIMENTAL INVESTIGATION OF THERMOMOLECULAR PRESSURE DIFFERENCE ON A THIN PERMEABLE NON-ISOTHERMAL MEMBRANE THERMOMOLECULAR PUMP
pp. 733-746
DOI: 10.1615/TsAGISciJ.2017019843
DEVELOPMENT OF THE CONCEPT OF CURVILINEAR CHANNELS FOR PROPULSION SYSTEM INLETS AND NOZZLES EMBEDDED IN THE AIRFRAME
pp. 747-758
DOI: 10.1615/TsAGISciJ.2017019841
METHOD OF IDENTIFICATION AND PREDICTION OF MOISTURE ABSORPTION BY POLYMER COMPOSITE MATERIALS DURING AGING
pp. 759-773
DOI: 10.1615/TsAGISciJ.2017019839
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