Sensitivity of flow visualization methods at low-density flow conditions.
Sensitivity limits of flow visualization methods using schlieren-interferometer techniques at low density flow conditions
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Sensitivity limits of flow visualization methods using schlieren-interferometer techniques at low density flow conditions
Flow oscillation incipience when subcooled liquid undergoes phase change under forced flow conditions in single-tube boiler
Through flow solution for axial flow turbomachine blade rows
Onset of flow oscillations when subcooled liquid undergoes phase change under forced flow in single tube boiler
Performance, inlet flow characteristics, and radiated noise measurement for turbojet engine with choked inlet flow
Visualization of turbulent flows by means of flow birefringence
A 30-inch tip-diameter axial-flow compressor stage was investigated with and without rotor to determine individual blade-row performance, interblade-row effects, and outer-wall boundary-layer conditions. Velocity gradients at guide-vane outlet without rotor approximated design assumptions, when the measured variation of leaving angle was considered. With rotor in operation, Mach number and rotor-blade effects changed flow distribution leaving guide vanes and invalidated design assumption of radial equilibrium. Rotor-blade performance correlated interpolated two-dimensional results within 2 degrees, although tip stall was indicated in experimental and not two-dimensional results. Boundary-displacement thickness was less than 1.0 and 1.5 percent of passage height after guide vanes and after rotor, respectively, but increased rapidly after rotor when tip stall occurred.
In many convective liquid-vapor phase change heat transfer engineering applications, cryogenic fluids are widely used in industrial processes, spacecraft and cryosurgery systems, and so on. For example, cryogens are usually used as liquid fuels such as liquid hydrogen and oxygen in the rocket industry, liquid nitrogen (LN2) and helium are frequently used to cool superconducting magnetic device for medical applications. In these systems, proper transport, handling, and storage of cryogenic fluids are of extreme importance. Among all the cryogenic transport processes performed in room temperatures, quenching, also termed chilldown, is a unavoidable initial, transient phase-change heat transfer process that brings the system down to the cryogenic condition. The Leidenfrost temperature or rewet temperature that signals the end of film boiling is practically considered the completion point of a quenching process. Therefore, rewet temperature has been considered the most important parameter for the engineering design of cryogenic thermal management systems. As most of the previous correlations for predicting the Leidenfrost temperature and the rewet temperature have been basically developed for water, they are shown to disagree with recent liquid nitrogen pipe chilldown experiments in upward and downward flow directions over a wide range of flow rates, pressures, and degrees of inlet subcooling. In addition to a complete review of the literature, two new correlations are presented in this work, one based on bubble growth and another based on the theoretical maximum limit of superheat. Each correlation performs well over the entire data set.
Nonequilibrium inviscid flow about arbitrarily shaped body with detached shock waves, using method with time derivative and bypassing boundary conditions
Incompressible laminar boundary layer development over two-dimensional symmetric body in presence of shear flow
Pressure coefficient criterion for transition between two- and three-dimensional turbulent cavity flow
Flow visualization and containment tests in directed-wall-jet vortex tube with radial outflow and moderate superimposed axial flows
Analytical investigation of flow and wall temperature sensitivity in heated passages for large inlet to exit density ratios in subsonic flow of nuclear rocket
Axial flow compressor design computer programs incorporating radial distribution of total pressure and flow path or axial velocity ratio
Supersonic jet noise generation by radial annular jet flow impinging on first shock cell region of axisymmetric converging main jet flow
Reduction of noise from underexpanded axisymmetric jet flows using radial jet flow impingement
Water vortex flow visualization to investigate flow stability and patterns in radial outflow vortices
Electron beam flow visualization technique for observing low density hypersonic He flows, confirming wing-shock body-shock system existence