1952 Steel Seizure Revisited - Systematic Study In Presidential Decision-Making

Managemen

Steady and Unsteady Flow Effects of Circumferential Grooves Casing Treatment in a Transonic Compressor Rotor

The current paper reports on an investigation of steady and unsteady flow effects of circumferential grooves casing treatment in a transonic compressor rotor. Circumferential grooves casing treatment is used mainly to increase stall margin in axial compressors with a relatively small decrease in aerodynamic efficiency. It is widely believed that flow mechanisms of circumferential grooves casing treatment near stall conditions are not yet well understood even though this treatment has been used widely in real engines. Numerical analysis based on steady Reynolds-averaged Navier-Stokes (RANS) has been the primary tool used to understand flow mechanism for circumferential grooves casing treatment. Although steady RANS explains some flow effects of circumferential grooves casing treatment, it does not calculate all the measured changes in the compressor characteristics. Therefore, design optimization of circumferential grooves with steady RANS has not been very successful. As a compressor operates toward the stall condition, the flow field becomes transient. Major sources of self-generated flow unsteadiness are shock oscillation and interaction between the passage shock and the tip leakage vortex. In the present paper, an unsteady Reynolds-averaged Navier-Stokes (URANS) approach is applied to study the effects of circumferential grooves in a transonic compressor. The results from URANS are compared with the results from RANS and measured data. The current investigation shows that there are significant unsteady flow effects on the performance of the circumferential grooves casing treatment. For the currently investigated rotor, the unsteady effects are of the same magnitude as the steady effects in terms of extending the compressor stall margin

Toward Optimum Configuration of Circumferential Groove Casing Treatment in Transonic Compressor Rotors

The current paper first reviews experimental and numerical investigations to understand flow physics and to develop optimum configurations of circumferential grooves in compressor rotors. Circumferential grooves are used mainly to increase stall margin in axial compressors with small decrease in aerodynamic efficiency. Although circumferential groove casing treatment has been used widely, flow mechanisms of the circumferential grooves at near stall conditions are not well understood yet. Detailed time-dependent flow measurement inside tip gap in a high speed compressor is still a big challenge even though significant advance has been made in non-intrusive flow measurement technique. Therefore numerical approaches have been used to study relevant flow physics. However, optimum design of circumferential grooves to a given compressor with the computational tools is not practical yet. In the present paper, various investigations to study flow physics of circumferential groove casing treatment in axial compressor are reviewed first. Possible missing flow physics are identified and future research efforts for the optimum design are discussed

High Power Laser - Plasma Interactions for Homeland Security Applications

Advance in laser technology over the last few decades have allowed progress in intense laser-plasma interaction research. The relativistic plasma generated by intense laser pulses can generate many different forms of radiation. This radiation, including X-rays, has been studied intensively due to the numerous potential applications of these sources. For example, for Homeland Security, radiation sources are already utilized to detect dangerous materials and hidden items that threaten civil safety. Neutrons and THz radiation have been studied as candidates for next generation screening, which may complement typical X-ray techniques. This thesis contains three experimental studies of high-power laser-plasma interactions as sources of radiation for Homeland Security applications, especially at kilohertz repetition-rates using few- millijoule pulses. First, a neutron generation experiment was conducted using a high repetition-rate laser system (1⁄2 kHz) at the University of Michigan. A heavy water (D2O) stream was irradiated by 40 fs pulses, each containing a few millijoules of energy. Acceleration of deuterons (to E < 1 MeV) was achieved through plasma sheath acceleration. Ensuing DD nuclear fusion reactions, in turn, generated neutron fluxes of up to 10^5 s^−1 into 4π steradians. In order to understand the neutron source characteristics, deuteron spectra were measured with CR39 detectors and compared to particle-in-cell (PIC) relativistic plasma dynamics simulations. The neutron source characteristics were analyzed using various neutron detection techniques, including Time-of-Flight measurements, bubble detectors, and neutron-capture gamma-ray measurements. Second, THz generation from laser filamentation in air was investigated. For security applications, THz can complement X-ray scanning, because THz can detect non-metallic materials and dangerous chemicals while not ionizing the sample. Even though there have been extensive studies on THz generation from laser filamentation processes, the exact generation mechanisms are yet to be determined. In this thesis, optimization of THz radiation using an adaptive optic with active feedback was demonstrated. Using a genetic algorithm, the THz radiation was improved six-fold without the need for detailed knowledge of the mechanisms. In particular, the use of a high repetition-rate laser system accelerated the optimization of the THz signal. Another strength of this optimization system is that it can enhance certain THz generation mechanisms depending on the experimental circumstances. Lastly, using a nanosecond pulsed high-power laser system (10 Hz), a long-range detection technique was developed for detection of special nuclear materials. Although direct detection of radiation from nuclear materials can be defeated by radiation shielding, leakage of radiation-ionized gases can provide an alternative indicator of the existence of nuclear materials. For instance, in the presence of ionizing radiation, the ratio of ionized nitrogen to neutral nitrogen would be higher than in no-source air-plasma conditions. By inducing optical breakdown (plasma) near a sample’s position, the ionization levels of the surrounding air were analyzed. To enhance the detection efficiency, an adaptive-optic feedback system was introduced with this ratio as a figure-of-merit. This resulted in a 50 % enhancement in the spectral ratio of the nitrogen lines. In addition, aerosol-initiated plasma spectra were distinguished from the original air-breakdown plasma, as a step toward practical deployment.PHDNuclear Engineering & Radiological SciencesUniversity of Michigan, Horace H. Rackham School of Graduate Studieshttps://deepblue.lib.umich.edu/bitstream/2027.42/145909/1/jmhah_1.pd

Compressor and fan wake characteristics

A triaxial probe and a rotating conventional probe, mounted on a traverse gear operated by two step motors were used to measure the mean velocities and turbulence quantities across a rotor wake at various radial locations and downstream stations. The data obtained was used in an analytical model developed to study how rotor flow and blade parameters and turbulence properties such as energy, velocity correlations, and length scale affect the rotor wake characteristics and its diffusion properties. The model, includes three dimensional attributes, can be used in predicting the discrete as well as broadband noise generated in a fan rotor, as well as in evaluating the aerodynamic losses, efficiency and optimum spacing between a rotor and stator in turbomachinery

Effects of Unsteady Flow Interactions on the Performance of a Highly-Loaded Transonic Compressor Stage

The primary focus of this paper is to investigate the loss sources in an advanced GE transonic compressor design with high reaction and high stage loading. This advanced compressor has been investigated both experimentally and analytically in the past. The measured compressor efficiency is significantly lower than the efficiency calculated with various existing tools based on RANS and URANS. The general understanding is that some important flow physics in this modern compressor design are not represented in the current tools. To pinpoint the source of the efficiency miss, an advanced test with detailed flow traverse was performed for the front one and a half stage at the NASA Glenn Research Center. In the present paper, a Large Eddy Simulation (LES) is employed to determine whether a higher-fidelity simulation can pick up any additional flow physics that can explain past efficiency miss with RANS and URANS. The results from the Large Eddy Simulation were compared with the NASA test results and the GE interpretation of the test data. LES calculates lower total pressure and higher total temperature on the pressure side of the stator, resulting in large loss generation on the pressure side of the stator. On the other hand, existing tools based on the RANS and URANS do not calculate this high total temperature and low total pressure on the pressure side of the stator. The calculated loss through the stator from LES seems to match the measured data and the GE data interpretation. Detailed examination of the unsteady flow field from LES indicates that the accumulation of high loss near the pressure side of the stator is due to the interaction of the rotor wake with the stator blade. The strong rotor wake interacts quite differently with the pressure side of the stator than with the suction side of the stator blade. The concave curvature on the pressure side of the stator blade increases the mixing of the rotor wake with the pressure side boundary layer significantly. On the other hand, the convex curvature on the suction side of the stator blade decreases the mixing and the suction side blade boundary layer remains thin. The jet velocity in the rotor wake in the stator frame seems to magnify the curvature effect in addition to inviscid redistribution of wake fluid toward the pressure side of the blade

Unsteady Loss in the Stator Due to the Incoming Rotor Wake in a Highly-Loaded Transonic Compressor

The present paper reports an investigation of unsteady loss generation in the stator due to the incoming rotor wake in an advanced GE transonic compressor design with a high-fidelity numerical method. This advanced compressor with high reaction and high stage loading has been investigated both experimentally and analytically in the past. The measured efficiency in this advanced compressor is significantly lower than the design intention/goal. The general understanding is that the current generation of compressor design/analysis tools miss some important flow physics in this modern compressor design. To pinpoint the source of the efficiency miss, an advanced test with a detailed flow traverse was performed for the front one and a half stage at the NASA Glenn Research Center. Detailed data-match analysis by GE identified an unexpected high loss generation in the pressure side of the stator passage. Higher total temperature and lower total pressure are measured near the pressure side of the stator. Various analyses based on the RANS and URANS of the compressor stage do not calculate the measured higher total temperature and lower total pressure on the pressure side of the stator. In the present paper, a Large Eddy Simulation (LES) is applied to find the fundamental mechanism of this unsteady loss generation in the stator due to the incoming rotor wake. The results from the LES were first compared with the NASA test results and the GE interpretation of the test data. LES calculates lower total pressure and higher total temperature on the pressure side of the stator, as the measured data showed, resulting in large loss generation on the pressure side of the stator. Detailed examination of the unsteady flow field from LES shows that the rotor wake, which has higher total temperature and higher total pressure relative to the free stream, interacts quite differently with the pressure side of the blade compared to the suction side of the blade. The higher temperature in the wake remains high as the wake passes through the pressure side of the blade. On the other hand, the total temperature diffuses as it passes through near the suction surface. For the presently investigated compressor, the classical intra-stator wake transport to the pressure side of the blade by the slip velocity in the wake seems to be minor. The main causes of this phenomenon are three-dimensional unsteady vortex interactions near the blade surface. The stabilizing effect of the concave curvature on the suction side keeps the rotor wake thin. On the other hand, the destabilizing effect of the convex curvature of the pressure side makes the rotor wake thicker, which results in a higher total temperature measurement at the stator exit. Additionally, wake stretching through the stator seems to contribute to the redistribution of the total temperature and the loss generation

Inside Out Apologetics: Engaging Cultural Narratives in Peninsular Malaysia

In the Western world, Christian apologists, missionaries, and thinkers who noticed the dangers of a cultural shift called postmodernism have developed many resources in recent years to engage it. This shift started from a time when it was impossible to not believe in God to one in which such faith is one among many possibilities. Meanwhile, extensive analyses of and apologetic engagement with the Eastern culture (Arabic, Confucian, and Southern Asian clusters) has been sidelined, with only limited resources to believers in those parts of the world. Unlike communities and cultures in the West, Eastern communities are shaped more by a sense of honor and shame than by individual reasoning, guilt, and innocence. Hence, a recent apologetic method, called the Inside Out method, developed by apologists Mark Allen and Josh Chatraw, is proposed to engage the prevailing cultural narratives found in the Eastern cultures, particularly in Peninsular Malaysia, a Southeast Asian country. This presentation will apply an Inside Out method within the Malaysian context to engage its cultural narratives of religious pluralism and filial piety. The paper shows how apologetic conversations can be framed with a non-Christian Malaysian. By identifying and challenging his or her take on pluralism and piety, the method invites him or her to consider how the Christian faith tells a better narrative, because the Gospel is the greatest narrative to be told