TsAGI Science Journal
Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
Volume 49, 2018 Numéro 3
DOI: 10.1615/TsAGISciJ.v49.i3
ON THE ASYMPTOTIC THEORY OF INTERACTION OF THE RUNNING PRESSURE PERTURBATION WITH THE BOUNDARY LAYER IN A SUPERSONIC FLOW
pp. 209-224
DOI: 10.1615/TsAGISciJ.2018027076
SELF-SIMILAR SOLUTIONS FOR VISCOUS COMPRESSIBLE GAS FLOW INSIDE A CONE
pp. 225-237
DOI: 10.1615/TsAGISciJ.2018027158
VOLUME-CENTERED DISCHARGE IN SUPERSONIC AIR FLOW AT CONCENTRATED PROPANE AND OXYGEN INJECTION TO THE DISCHARGE ZONE
pp. 251-262
DOI: 10.1615/TsAGISciJ.2018027083
EFFECT OF MODEL ATTACHMENT BRACKETS FOR THE AV-102 MEASUREMENT SYSTEM ON THE RESULTS OF EXPERIMENTAL INVESTIGATIONS IN THE TSAGI T-102 WIND TUNNEL
pp. 263-272
DOI: 10.1615/TsAGISciJ.2018027068
DETERMINING ADMISSIBLE RANGE LIMITS FOR MOUNTING AIR SIGNAL SYSTEM SENSORS
pp. 273-287
DOI: 10.1615/TsAGISciJ.2018027046
ACTIVE FLUTTER SUPPRESSION OF A HIGH ASPECT RATIO WING AIRCRAFT
pp. 289-297
DOI: 10.1615/TsAGISciJ.2018027114
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