TsAGI Science Journal
Published 6 issues per year
ISSN Print: 1948-2590
ISSN Online: 1948-2604
Volume 51, 2020 Issue 5
DOI: 10.1615/TsAGISciJ.v51.i5
IVAN VLADIMIROVICH EGOROV (ON HIS 60TH BIRTHDAY)
The Editorial Board
The Editorial Board
pp. v-vi
DOI: 10.1615/TsAGISciJ.2021037744
NUMERICAL SOLUTION OF THE ASYMPTOTIC PROBLEM OF A FLOW NEAR A LOCAL ROUGHNESS
pp. 445-457
DOI: 10.1615/TsAGISciJ.2021037786
APPLICATION OF CLASSICAL TRAJECTORY METHOD OF MOLECULAR COLLISIONS FOR CALCULATING TRANSPORT COEFFICIENTS AND STUDYING THE RAREFIED GAS OUTFLOW INTO VACUUM
pp. 459-477
DOI: 10.1615/TsAGISciJ.2021037719
PHYSICAL CAUSES OF DIFFERENCES IN EFFECTIVENESS OF UPPER AND LOWER FINS AT SUPERSONIC SPEEDS
pp. 495-513
DOI: 10.1615/TsAGISciJ.2021037731
THE LAMINAR-TURBULENT TRANSITION STUDIES ON THE CONE SURFACE AT HIGH MACH NUMBERS BY THE NUMERICAL METHOD WITH BUILT-IN EMPIRICAL CRITERIA
pp. 515-530
DOI: 10.1615/TsAGISciJ.2021037713
ON DETERMINATION OF INTERNAL DRAG WHEN TESTING MODELS OF INTEGRATED AIRCRAFT WITH DUCTS
pp. 531-543
DOI: 10.1615/TsAGISciJ.2021037767
EXPERIMENTAL MODEL STUDIES OF THE EFFECTS OF JET FLOWS ON THE LAUNCH VEHICLE AND LAUNCH PAD WITH A SHORT EXHAUST CHANNEL
pp. 545-562
DOI: 10.1615/TsAGISciJ.2021037773
TECHNIQUE FOR HIGH-TEMPERATURE VACUUM TESTS OF HEAT-SHIELDING STRUCTURAL ELEMENTS
pp. 563-571
DOI: 10.1615/TsAGISciJ.2021037751
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