TsAGI Science Journal
Published 6 issues per year
ISSN Print: 1948-2590
ISSN Online: 1948-2604
Volume 48, 2017 Issue 8
DOI: 10.1615/TsAGISciJ.v48.i8
CONTROL OF VORTEX FLOW OVER A MANEUVERABLE AIRCRAFT MODEL USING NOSE FLAPS AT LARGE ANGLES OF ATTACK
pp. 699-709
DOI: 10.1615/TsAGISciJ.2018026350
MIXING LAYER STRUCTURE OF A JET IN A WIND TUNNEL WITH AN OPEN TEST SECTION
pp. 711-722
DOI: 10.1615/TsAGISciJ.2018026655
NONCONTACT MEASUREMENTS OF WING BOX DEFORMATION DURING STRENGTH TESTS BY VIDEOGRAMMETRY METHOD
pp. 751-760
DOI: 10.1615/TsAGISciJ.2018026351
TASKS OF THE MODAL TEST AND REPRODUCTION OF FORCES BY MEANS OF ELECTROMECHANICAL SIMULATION
pp. 761-771
DOI: 10.1615/TsAGISciJ.2018026703
BEAM STIFFNESSES OF A COMPOSITE WING WITH ANISOTROPIC SKIN
pp. 773-787
DOI: 10.1615/TsAGISciJ.2018026632
Latest Issue
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