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 46, 2015 册 7
DOI: 10.1615/TsAGISciJ.v46.i7
INFLUENCE OF HIGH-BYPASS-RATIO TURBOFAN JETS ON AERODYNAMIC CHARACTERISTICS OF HIGH-LIFT WING
pp. 619-629
DOI: 10.1615/TsAGISciJ.v46.i7.10
OPTIMIZATION OF THE FOREBODY OF A SUPERSONIC FLYING VEHICLE CONFIGURATION WITH A WINDWARD INTAKE
pp. 631-646
DOI: 10.1615/TsAGISciJ.v46.i7.20
PARAMETRIC DESCRIPTION OF THE AIRFOIL USING COMBINED POLYNOMIAL FUNCTIONS FOR OPTIMIZATION APPLICATIONS
pp. 647-656
DOI: 10.1615/TsAGISciJ.v46.i7.30
ONE SOLUTION OF THE NAVIER−STOKES EQUATIONS: SPHERICALLY SYMMETRIC POINT SOURCE IN A COMPRESSIBLE PERFECT GAS
pp. 657-670
DOI: 10.1615/TsAGISciJ.v46.i7.40
CRITERION TO SELECT OPTIMUM VALUES OF AIRCRAFT LATERAL STATIC STABILITY MARGIN IN LANDING APPROACH
pp. 671-686
DOI: 10.1615/TsAGISciJ.v46.i7.50
INVESTIGATION OF CRACK PROPAGATION PROCESS BY MEASUREMENTS OF LOCAL DEFORMATION RESPONSE: I. ACTUAL STRESS FIELD
pp. 687-714
DOI: 10.1615/TsAGISciJ.v46.i7.60
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