Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Electrical Engineering and Computer Science, 1981. / MICROFICHE COPY AVAILABLE IN ARCHIVES AND ENGINEERING / Includes bibliographical references. / by Scott Roger Shepard. / M.S.

Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Electrical Engineering and Computer Science, 1981. / MICROFICHE COPY AVAILABLE IN ARCHIVES AND ENGINEERING. / Includes bibliographical references. / by Peter Vickers Wright. / Ph.D.

Thesis. 1975. Ph.D.--Massachusetts Institute of Technology. Dept. of Electrical Engineering and Computer Science. / Vita. / Includes bibliographies. / Ph.D.

Li Xin. / Thesis (M.Phil.)--Chinese University of Hong Kong, 2003. / Includes bibliographical references (leaves 81-86). / Abstracts in English and Chinese. / COHERENT OPTICAL CODE DIVISION MULTIPLE ACCESS BASED ON SUPERSTRUCTURE FIBER BRAGG GRATING ENCODERS AND DECODERS --- p.1 / ACKNOWLEDGEMENT --- p.2 / ABSTRACT --- p.III / 摘要 --- p.V / CONTENTS --- p.VI / LIST OF FIGURES --- p.1 / Chapter CHAPTER 1 --- INTRODUCTION --- p.3 / Chapter 1.1 --- Overview of OCDMA --- p.3 / Chapter 1.2 --- Classification of OCDMA Schemes --- p.6 / Chapter 1.3 --- Introduction of Coherent OCDMA Schemes --- p.9 / Chapter 1.4 --- Introduction of superstructure Fiber Bragg Gratings and Other Encoding and Decoding Components --- p.10 / Chapter 1.5 --- Outline of the Thesis --- p.13 / Chapter CHAPTER 2 --- COUPLED MODE THEORY AND SUPERSTRUCTURE FIBER BRAGG GRATING SIMULATION MODEL --- p.16 / Chapter 2.1 --- Fiber Bragg Grating Model Based on Coupled Mode Theory --- p.16 / Chapter 2.1.1 --- Introduction of FBG and the Coupled Mode Theory --- p.16 / Chapter 2.1.2 --- FBG Model Based on CMT --- p.18 / Chapter 2.1.3 --- FBG Model When there are Phase Discontinuities Between Different Parts --- p.20 / Chapter 2.2 --- Properties of Fiber Bragg Gratings --- p.22 / Chapter 2.3 --- Simulation Model of superstructure Fiber Bragg Gratings --- p.27 / Chapter 2.4 --- Summary --- p.31 / Chapter CHAPTER 3 --- COHERENT OCDMA CODING SCHEME BASED ON THE SUPERSTRUCTURE FIBER BRAGG GRATING ENCODER/DECODER --- p.33 / Chapter 3.1 --- Introduction and Theoretical Derivation of the Coding Scheme --- p.33 / Chapter 3.1.1 --- Introduction of the Coding Scheme --- p.33 / Chapter 3.1.2 --- Derivation of SSFBG Encoder --- p.34 / Chapter 3.1.3 --- Encoding for the SSFBG --- p.39 / Chapter 3.2 --- Introduction of the Simulation Model and the Research on It …… --- p.44 / Chapter 3.3 --- Summary --- p.47 / Chapter CHAPTER 4 --- RESEARCH ON THE SIMULATED COHERENT OCDMA SYSTEM IN IDEAL CASE --- p.48 / Chapter 4.1 --- Introduction of the ideal case and factors that affect the system performance --- p.48 / Chapter 4.2 --- Effects by Refractive Index Modulation of the SSFBG Encoder --- p.49 / Chapter 4.3 --- Effects by Code Type --- p.54 / Chapter 4.4 --- Effect by the Code Length --- p.57 / Chapter 4.5 --- Summary --- p.60 / Chapter CHAPTER 5 --- RESEARCH ON THE SIMULATED COHERENT OCDMA SYSTEM IN PRACTICAL ENVIRONMENT --- p.62 / Chapter 5.1 --- Introduction --- p.62 / Chapter 5.2 --- Comparison of System Performance in Synchronous and Asynchronous Cases --- p.63 / Chapter 5.3 --- Discussion on the System Performance When Users are In Different Power Levels --- p.65 / Chapter 5.4 --- Analysis of Channel Noise In the Coherent OCDMA System --- p.68 / Chapter 5.5 --- Summary --- p.70 / Chapter CHAPTER 6 --- CONCLUSIONS AND FUTURE WORK --- p.72 / Chapter 6.1 --- Conclusions --- p.72 / Chapter 6.2 --- Future Work --- p.75 / APPENDIX A PROOF OF SSFBG THEORETICAL MODEL APPROXIMATION --- p.77 / "APPENDIX B RANDOM SEQUENCE, M-SEQUENCE AND WALSH SEQUENCE" --- p.80 / REFERENCES --- p.81

Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1981. / Microfiche copy available in Archives and Barker. / Includes bibliographical references. / by Steven James Hollowell. / M.S.

The concern of this thesis was to investigate the nonlinear dynamics inherent in oscillating waterfalls.

Abstract not available

For thesis abstract select View Thesis Title, Contents and Abstract

<p>This research presents the detailed investigation of coupled-mode flutter and non-synchronous vibration in turbomachinery. Coupled-mode flutter and non-synchronous vibration are two aeromechanical challenges in designing turbomachinery that, when present, can cause engine blade failure. Regarding flutter, current industry design practices calculate the aerodynamic loads on a blade due to a single mode. In response to these design standards, a quasi three-dimensional, reduced-order modeling tool was developed for identifying the aeroelastic conditions that cause multi-mode flutter. This tool predicts the onset of coupled-mode flutter reasonable well for four different configurations, though certain parameters were tuned to agree with experimentation. Additionally, the results of this research indicate that mass ratio, frequency separation, and solidity have an effect on critical rotor speed for flutter. Higher mass-ratio blades require larger rotational velocities before they experience coupled-mode flutter. Similarly, increasing the frequency separation between modes and raising the solidity increases the critical rotor speed. Finally, and most importantly, design guidelines were generated for defining when a multi-mode flutter analysis is required in practical turbomachinery design. </p><p>Previous work has shown that industry computational fluid dynamics can approximately predict non-synchronous vibration (NSV), but no real understanding of frequency lock-in and blade limit-cycle amplitude exists. Therefore, to understand the causes of NSV, two different reduced-order modeling approaches were used. The first approach uses a van der Pol oscillator to model a non-linear fluid instability. The van der Pol model is then coupled to a structural degree of freedom. This coupled system exhibits the two chief properties seen in experimental and computational non-synchronous vibration. Under various conditions, the fluid instability and the natural structural frequency will lock-in, causing structural limit-cycle oscillations. This research shows that with proper model-coefficient choices, the frequency range of lock-in can be predicted and the conditions for the worst-case, limit-cycle-oscillation amplitude can be determined. This high-amplitude limit-cycle oscillation is found at an off-resonant condition, i.e., the ratio of the fluid-shedding frequency and the natural-structural frequency is not unity. In practice, low amplitude limit-cycle oscillations are acceptable; this research gives insight into when high-amplitude oscillations may occur and suggests that altering a blade's natural frequency to avoid this resonance can potentially make the response worse.</p><p>The second reduced-order model uses proper orthogonal decomposition (POD) methods to first reconstruct, and ultimately predict, computational fluid dynamics (CFD) simulations of non-synchronous vibration. Overall, this method was successfully developed and implemented, requiring between two and six POD modes to accurately predict CFD solutions that are experiencing non-synchronous vibration. This POD method was first developed and demonstrated for a transversely-moving, two-dimensional cylinder in cross-flow. Later, the method was used for the prediction of CFD solutions for a two-dimensional compressor blade, and the reconstruction of solutions for a three-dimensional first-stage compressor blade. </p><p>This research is the first to offer a van der Pol or proper orthogonal decomposition approach to the reduced-order modeling of non-synchronous vibration in turbomachinery. Modeling non-synchronous vibration is especially challenging because NSV is caused by complicated, unsteady flow dynamics; this initial study helps researchers understand the causes of NSV, and aids in the future development of predictive tools for aeromechanical design engineers.</p> / Dissertation

Thesis (Ph. D.)--Oregon State University, 1993. / Typescript (photocopy). Includes bibliographical references (leaves 102-110). Also available on the World Wide Web.