The stability of a steady, vortical flow in a cylindrical container with one rotating endwall has been experimentally examined to gain insight into the process of vortex breakdowwn. The dynamics of the flow are governed by the Reynolds number (Re) and the aspect ratio of the cylinder. Re is given by Omega R(sup 2)/nu, where Omega is the speed of rotation of the endwall, R is the cylinder radius, and nu is the kinematic viscosity of the fluid filling the cylinder. The aspect ratio is H/R, where H is the height of the cylinder. Numerical simulation studies disagree whether or not the steady breakdown is stable beyond a critical Reynolds number, Re(sub c). Previous experimental researches have considered the steady and unsteady flows near Re(s...
The flow through the exhaust nozzle of a jet engine has been of crucial importance in aerospace appl...
Accurately modeling the transfer of mass, momentum, and energy through engine near-wall regions is c...
Viscous transonic flows at large Reynolds numbers over 3-D wings were analyzed using a zonal viscid-...
The effects of active flow control by oscillatory blowing at the leading edge of a nonslender delta ...
Flow-visualization studies of ogival, parabolic, and conical forebodies were made in a comprehensive...
H2O time-histories were studied within the H2/O2 system using a tunable diode laser system and a pre...
The objective of this investigation is experimental and computational study of three dimensional vis...
An experimental investigation is reported on slanted base ogive cylinders at zero incidence. The Mac...
This study is motived by the dynamic stall of rotorcraft blades. Dynamic stall is an attribute of ai...
The counter-rotating pair of wake vortices shed by flying aircraft can pose a threat to ensuing airc...
Experimental crosswire measurements of the flowfield above a 70 and 75 degree flat plate delta wing ...
Merger of vortices is examined experimentally to compare the merger of slender parallel vortices gen...
Structures conveying mass lose stability once the mass exceeds a certain critical velocity. The typ...
A specially designed wind tunnel was used to examine the effects of tandemly arranged parallel plate...
Dynamic stall occurs in applications where airfoils are rapidly changing angle of attack, like rotor...
The flow through the exhaust nozzle of a jet engine has been of crucial importance in aerospace appl...
Accurately modeling the transfer of mass, momentum, and energy through engine near-wall regions is c...
Viscous transonic flows at large Reynolds numbers over 3-D wings were analyzed using a zonal viscid-...
The effects of active flow control by oscillatory blowing at the leading edge of a nonslender delta ...
Flow-visualization studies of ogival, parabolic, and conical forebodies were made in a comprehensive...
H2O time-histories were studied within the H2/O2 system using a tunable diode laser system and a pre...
The objective of this investigation is experimental and computational study of three dimensional vis...
An experimental investigation is reported on slanted base ogive cylinders at zero incidence. The Mac...
This study is motived by the dynamic stall of rotorcraft blades. Dynamic stall is an attribute of ai...
The counter-rotating pair of wake vortices shed by flying aircraft can pose a threat to ensuing airc...
Experimental crosswire measurements of the flowfield above a 70 and 75 degree flat plate delta wing ...
Merger of vortices is examined experimentally to compare the merger of slender parallel vortices gen...
Structures conveying mass lose stability once the mass exceeds a certain critical velocity. The typ...
A specially designed wind tunnel was used to examine the effects of tandemly arranged parallel plate...
Dynamic stall occurs in applications where airfoils are rapidly changing angle of attack, like rotor...
The flow through the exhaust nozzle of a jet engine has been of crucial importance in aerospace appl...
Accurately modeling the transfer of mass, momentum, and energy through engine near-wall regions is c...
Viscous transonic flows at large Reynolds numbers over 3-D wings were analyzed using a zonal viscid-...