TsAGI Science Journal
Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
Volume 45, 2014 Numéro 7
DOI: 10.1615/TsAGISciJ.v45.i7
NOZZLE THRUST AUGMENTATION UNDER DIMENSIONAL CONSTRAINTS
pp. 571-579
DOI: 10.1615/TsAGISciJ.2014012538
METHODOLOGY AND EXAMPLES OF NUMERICAL INVESTIGATIONS OF BODIES WITH DUCTS AT SUPERSONIC FLOW VELOCITIES
pp. 581-598
DOI: 10.1615/TsAGISciJ.2014012837
INTERFERENCE CONCEPT OF AERODYNAMIC DESIGN OF EFFECTIVE HYPERSONIC CONFIGURATIONS
pp. 599-617
DOI: 10.1615/TsAGISciJ.2014012528
INTERACTION OF A SUPERSONIC JET HEAVY LOADED BY PARTICLES WITH A SOLID BODY
pp. 619-638
DOI: 10.1615/TsAGISciJ.2015013277
FUEL CONSUMPTION MINIMIZATION FOR AGRICULTURAL AIRCRAFT CONDUCTING SPRAYING
pp. 639-657
DOI: 10.1615/TsAGISciJ.2015013290
EXPERIMENTAL INVESTIGATION OF THE AEROGASDYNAMICS OF A VECTORED-THRUST NOZZLE
pp. 659-667
DOI: 10.1615/TsAGISciJ.2014012972
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