TsAGI Science Journal
Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
Volume 40, 2009 Numéro 5
DOI: 10.1615/TsAGISciJ.v40.i5
STUDY OF AERODYNAMICS OF THE AEROSPACE VEHICLE WITH A DEFLECTED BALANCING FLAP
pp. 517-534
DOI: 10.1615/TsAGISciJ.v40.i5.10
LIFT AND INDUCED DRAG OF A FINITE-SPAN WING IN A FLOW OF VISCOUS COMPRESSIBLE GAS AT SUBSONIC SPEEDS
pp. 535-551
DOI: 10.1615/TsAGISciJ.v40.i5.20
ON THE UNSTEADY FLUID FLOWS IN DOMAINS WITH CLOSED STREAMLINES
pp. 553-560
DOI: 10.1615/TsAGISciJ.v40.i5.30
NOSE PARTS OF MINIMAL WAVE DRAG WITH THE FRONT FACE AND THE POWER-LAW GENEATRIX
pp. 561-569
DOI: 10.1615/TsAGISciJ.v40.i5.40
COMPARISON OFTHE RESULTS OF NUMERICAL CALCULATIONS BY THE METHOD BASED ON THE GODUNOV-KOLGAN-RODIONOV DIFFERENCE SCHEME WITH THE EXPERIMENTAL DATA FOR THE TRANSONIC FLOW AROUND RAE 2822 AIRFOIL
pp. 571-585
DOI: 10.1615/TsAGISciJ.v40.i5.50
ABOUT THE SECONDARY SEPARATION AT SUPERSONIC FLOW OVER A COMPRESSION RAMP
pp. 587-607
DOI: 10.1615/TsAGISciJ.v40.i5.60
STUDY OF VISCOUS−INVISCID INTERACTION ON AN OSCILLATING MODEL OF AN AIRPLANE WITH A SWEPT WING
pp. 609-617
DOI: 10.1615/TsAGISciJ.v40.i5.70
RESEARCH ON THERMAL DYNAMICS OF STRAIN-GAUGE BALANCE AND DEVELOPMENT OF METHODS FOR ITS TEMPERATURE ERROR REDUCTION
pp. 619-629
DOI: 10.1615/TsAGISciJ.v40.i5.80
COMPOUND TRIANGULAR FINITE ELEMENT WITH CUBIC POLYNOMIAL FOR LATERAL PLATE BENDING
pp. 631-640
DOI: 10.1615/TsAGISciJ.v40.i5.90
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