TsAGI Science Journal
Publicado 6 números por año
ISSN Imprimir: 1948-2590
ISSN En Línea: 1948-2604
EFFECTS OF MASS TRANSFER ON PROPAGATION OF DISTURBANCES IN A HYPERSONIC FLOW OVER THE WING WITH POINT OF INFLECTION OF A LEADING EDGE
Volumen 45,
Edición 5, 2014,
pp. 431-450
DOI: 10.1615/TsAGISciJ.2014012226
SINOPSIS
The flow in a three-dimensional laminar boundary layer on a thin wing with a point of inflection of the leading edge is investigated in the case of strong viscous−inviscid interaction. The propagation of induced pressure disturbances is considered on the basis of the analysis of characteristic surfaces. Numerical solutions to the equations of the boundary layer on thin semi-infinite wings in a hypersonic flow of a viscous gas are found. The velocities of propagation of disturbances at different mass transfer rates on the wing surface, different temperature factors, and leading-edge sweep angles are determined.
PALABRAS CLAVE: flat wing, boundary layer, hypersonic flow, strong interaction, propagation of disturbances, mass transfer
338 Vistas de artículos
10 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