TsAGI Science Journal
Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
Volume 40, 2009 Numéro 4
DOI: 10.1615/TsAGISciJ.v40.i4
SEVERAL ASPECTS OF GAS FLOW WITH PRESCRIBED DISTRIBUTION OF HEAT SOURCES
pp. 401-417
DOI: 10.1615/TsAGISciJ.v40.i4.10
MONOTONIZATION OF THE FINITE ELEMENT METHOD IN THE PROBLEMS OF GAS DYNAMICS
pp. 419-436
DOI: 10.1615/TsAGISciJ.v40.i4.20
AERODYNAMIC CHARACTERISTICS OF MODELS OF VERTICAL TAKE-OFF AIRCRAFT (TILTROTOR) FOR A WIDE RANGE OF ANGLESOF ATTACK
pp. 437-452
DOI: 10.1615/TsAGISciJ.v40.i4.30
ANALYSIS OF THE SONIC BOOM INTENSITY USING NEAR-FIELD PERTURBATION UNDER THE AIRCRAFT, CALCULATED BY MEANS OF THE NONLINEAR THEORY
pp. 459-473
DOI: 10.1615/TsAGISciJ.v40.i4.50
NUMERIC INVESTIGATION OF THE VENTILATION SYSTEM OF AN ADVANCED AIRCRAFT PASSENGER CABIN
pp. 475-483
DOI: 10.1615/TsAGISciJ.v40.i4.60
A METHOD FOR TAKING INTO ACCOUNT THE INFLUENCE OF THE MODEL AND DYNAMOMETER WEIGHTS ON THE STRAIN-GAUGE BALANCE READINGS
pp. 485-495
DOI: 10.1615/TsAGISciJ.v40.i4.70
APPLICATION OF SIMILARITY TRANSFORMATION UPON PARAMETRIC INVESTIGATIONS OF FLUTTER
pp. 497-506
DOI: 10.1615/TsAGISciJ.v40.i4.80
AN ENGINEERING METHOD FOR DETERMINING CHARACTERISTICS OF A PROTECTIVE SCREEN AT IMPACT OF A NONLOCALIZED ENGINE FRAGMENT
pp. 507-516
DOI: 10.1615/TsAGISciJ.v40.i4.90
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