TsAGI Science Journal
Published 6 issues per year
ISSN Print: 1948-2590
ISSN Online: 1948-2604
Volume 43, 2012 Issue 4
DOI: 10.1615/TsAGISciJ.v43.i4
FLOW-FIELD CHARACTERISTICS IN A TURBULENT JET: EXPERIMENTAL DETERMINATION OF SOUND SOURCE LOCATIONS
pp. 401-423
DOI: 10.1615/TsAGISciJ.2012006678
MODIFICATION OF THE GODUNOV NUMERICAL METHOD FOR GAS-DYNAMICS EQUATIONS
pp. 425-438
DOI: 10.1615/TsAGISciJ.2012006697
INTERACTION OF SHORT-WAVE ACOUSTIC DISTURBANCES WITH A SHOCK WAVE ON A WEDGE IN HYPERSONIC FLOW
pp. 439-453
DOI: 10.1615/TsAGISciJ.2012006112
MECHANISMS OF NON-STATIONARY PROCESSES IN A LENGTHY CAVERN
pp. 445-480
DOI: 10.1615/TsAGISciJ.2012006703
EXPERIMENTAL INVESTIGATION OF THE INFLUENCE OF VORTEX GENERATORS AND LIQUID INJECTION ON NOISE IN HIGH-SPEED JETS
pp. 481-496
DOI: 10.1615/TsAGISciJ.2012006603
METHODOLOGY FOR TURBOMACHINERY NOISE ANALYSIS BASED ON A NUMERICAL MODEL OF PROPAGATION
pp. 515-531
DOI: 10.1615/TsAGISciJ.2012006684
NUMERICAL CALCULATION OF ACOUSTIC PROPERTIES OF LINERS
pp. 533-547
DOI: 10.1615/TsAGISciJ.2012006586
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