TsAGI Science Journal
Publication de 6 numéros par an
ISSN Imprimer: 1948-2590
ISSN En ligne: 1948-2604
Volume 51, 2020 Numéro 1
DOI: 10.1615/TsAGISciJ.v51.i1
AN INVERSE DESIGN METHOD FOR A WING IN FULL CRUISING CONFIGURATION OF A REGIONAL AIRCRAFT VIA RANS APPROACH
pp. 1-13
DOI: 10.1615/TsAGISciJ.2020034077
DEVELOPMENT, VERIFICATION, AND VALIDATION OF THE METHODOLOGY FOR SONIC BOOM OVERPRESSURE AND LOUDNESS CALCULATION USING MODERN COMPUTATIONAL FLUID DYNAMICS METHODS
pp. 15-28
DOI: 10.1615/TsAGISciJ.2020034238
ABOUT THE BODY OF REVOLUTION OF MINIMUM DRAG WITH A CYLINDRICAL CENTRAL PORTION
pp. 29-36
DOI: 10.1615/TsAGISciJ.2020034176
CALCULATION OF ACOUSTIC CHARACTERISTICS OF A JET FROM A RECTANGULAR NOZZLE WITH ESTIMATION OF EFFECT OF THE PLATE ADJACENT TO ITS EXIT SECTION
pp. 37-54
DOI: 10.1615/TsAGISciJ.2020034256
EXPERIMENTAL INVESTIGATION OF AEROTHERMODYNAMIC CHARACTERISTICS OF THE EXOMARS PROJECT LANDER AT HYPERSONIC VELOCITIES
pp. 55-61
DOI: 10.1615/TsAGISciJ.2020034055
ASSESSMENT OF THE POSSIBILITY OF NEAR-RESONANT ROTATION MODES DURING UNCONTROLLED DESCENT OF SPENT LAUNCH VEHICLE BOOSTERS IN THE ATMOSPHERE
pp. 63-84
DOI: 10.1615/TsAGISciJ.2020034137
PANEL FLUTTER OF PLATE UNDER SUBSONIC FLOW IN TWO-DIMENSIONAL APPROACH
pp. 85-98
DOI: 10.1615/TsAGISciJ.2020034274
CALCULATION OF EQUIVALENT TRANSVERSAL SHEAR MODULES OF A LAYERED COMPOSITE PACKAGE
pp. 99-110
DOI: 10.1615/TsAGISciJ.2020034234
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