TsAGI Science Journal
Publicado 6 números por año
ISSN Imprimir: 1948-2590
ISSN En Línea: 1948-2604
TRANSONIC CROSS FLOW (M∞ = 0.8) OVER A CIRCULAR CYLINDER AT HIGH REYNOLDS NUMBERS
Volumen 43,
Edición 5, 2012,
pp. 589-613
DOI: 10.1615/TsAGISciJ.2013006844
SINOPSIS
On the basis of the Navier-Stokes and the Reynolds equations the numerical simulation of a transonic perfect gas cross flow over a circular cylinder with a thermally insulated surface at the Mach number M∞ = 0.8 and the Reynolds numbers 103 ≤ Re ≤ 107 is performed. An effect of the Reynolds number on the structure of the flow field, the flow regime, and aerodynamic characteristics of the cylinder is demonstrated.
5211 Vistas de artículos
18 Descargas de artículos
Métrica
Artículos con contenido similar:
Último edicion
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