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Dissertations / Theses on the topic 'Rotor flows'

Author: Grafiati

Published: 3 June 2025

Last updated: 20 July 2025

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1

Dehaeze, Florent. "Aeroelastic analysis of turbulent rotor flows." Thesis, University of Liverpool, 2012. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.570227.

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This thesis is devoted to the study of rotor flows. A literature survey suggested that possible improvements can be achieved via better simulation of turbulence and prediction of the elastic blade de- formation. While the limits of the currently used URANS turbulence models have been shown, accurate predictions can only be achieved if the blade elasticity is taken account due to the large deformations a rotor blade can undergo in flight. An aeroelastic coupling strategy consists in three steps: computing the flow field, computing the structural deformation and transferring data between the CFD

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2

Berkman, Mert Enis. "An integrated Navier Stokes-full portential-free wake method for rotor flows." Diss., Georgia Institute of Technology, 1998. http://hdl.handle.net/1853/12388.

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3

Lee, Betty. "Dynamic response of small turbine flowmeters in pulsating liquid flows." Thesis, Brunel University, 2002. http://bura.brunel.ac.uk/handle/2438/4971.

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The dynamic response of turbine flowmeters in low pressure gas flows (i. e. where the rotational inertia of the fluid is negligible) is well understood and methods for correcting meter signals for a lack of response are available. For liquid flows there has been a limited amount of experimental work on the response of meters to step changes but no reports have been found of the response of meters to sinusoidally pulsating flows. "Small" turbine meters are expected to behave differently from "large" meters for a number of reasons: a smaller meter would generally have: (1) a larger percentage of

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4

Wang, Chun-Wei. "Prediction of turbine cascade flows with a quasi-three-dimensional rotor viscous code and the extension of the algebraic turbulence model." Thesis, Monterey, California. Naval Postgraduate School, 1992. http://hdl.handle.net/10945/24012.

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Approved for public release; distribution is unlimited<br>A quasi- three-dimensional rotor viscous code is used to predict high subsonic flow through an annular cascade of turbine blades. The well known Baldwin- Lomax turbulence model is used in the program. An attempt was made to implement a new turbulence model, based on renormalization group theory in the program. This was done to improve the prediction of the boundary layer transition on the blade surfaces . and subsequent wake development. The comparison of these two turbulence models with experimental data are presented. Pressure

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5

Arisi, Allan Nyairo. "Heat Transfer and Flow Characteristics on the Rotor Tip and Endwall Platform Regions in a Transonic Turbine Cascade." Diss., Virginia Tech, 2016. http://hdl.handle.net/10919/64501.

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This dissertation presents a detailed experimental and numerical analysis of the aerothermal characteristics of the turbine extremity regions i.e. the blade tip and endwall regions. The heat transfer and secondary flow characteristics were analyzed for different engine relevant configurations and exit Mach/Reynolds number conditions. The experiments were conducted in a linear blowdown cascade at transonic high turbulence conditions of Mexit ~ 0.85, 0.60 and 1.0, with an inlet turbulence intensity of 16% and 12% for the vane and blade cascade respectively. Transient infrared (IR) thermography t

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6

Peres, Noele. "A 3D pseudospectral method for cylindrical coordinates. Application to the simulations of rotating cavity flows." Thesis, Aix-Marseille, 2012. http://www.theses.fr/2012AIXM4309/document.

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La simulation d'écoulements dans des cavités cylindriques en rotation présente une difficulté particulière en raison de l'apparition de singularités sur l'axe. Le présent travail propose une méthode collocative pseudospectrale suffisamment efficace et précise pour surmonter cette difficulté et résoudre les équations 3D de Navier-Stokes écrites en coordonnées cylindriques. Cette méthode a été développée dans le cadre des différentes études menées au laboratoire M2P2, utilisant une méthode collocative de type Chebychev dans les directions radiale et axiale et Fourier-Galerkin dans la direction a

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7

Courtiade, Nicolas. "Experimental analysis of the unsteady flow and instabilities in a high-speed multistage compressor." Phd thesis, Ecole Centrale de Lyon, 2012. http://tel.archives-ouvertes.fr/tel-00838695.

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The present work is a result of collaboration between the LMFA (Laboratoire de Mécanique des Fluides et d'Acoustique, Ecole Centrale de Lyon - France), Snecma and the Cerfacs. It aims at studying the flow in the 3.5-stages high-speed axial compressor CREATE (Compresseur de Recherche pour l'Etude des effets Aérodynamique et TEchnologique - rotation speed: 11543 RPM, Rotor 1 tip speed: 313 m/s), designed and built by Snecma and investigated at LMFA on a 2-MW test rig. Steady measurements, as well as laser velocimetry, fast-response wall static and total pressure measurements have been used to ex

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8

Gougeon, Pierre. "Interactions aérodynamiques entre une turbine haute pression et le premier distributeur basse pression." Thesis, Ecully, Ecole centrale de Lyon, 2014. http://www.theses.fr/2014ECDL0026/document.

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L’amélioration des performances des turboréacteurs actuels est un enjeu crucial dans un contexte de contraintes économiques et environnementales fortes. Au sein du turboréacteur, le canal inter-turbines, localisé à l’interface entre la turbine Haute Pression (HP) et le premier distributeur Basse Pression (BP), est le siège d’écoulements très complexes. Ainsi, les structures aérodynamiques issues de la turbine HP (sillages, tourbillons et ondes de choc) interagissent fortement entre elles et impactent l’écoulement du distributeur BP, engendrant ainsi des pertes de rendement de l’ensemble de la

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9

Vasilescu, Roxana. "Helicopter blade tip vortex modifications in hover using piezoelectrically modulated blowing." Diss., Available online, Georgia Institute of Technology, 2004:, 2004. http://etd.gatech.edu/theses/available/etd-11192004-165246/unrestricted/vasilescu%5Froxana%5F200412%5Fphd.pdf.

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Thesis (Ph. D.)--Aerospace Engineering, Georgia Institute of Technology, 2005.<br>Dancila, Stefan, Committee Chair ; Sankar, Lakshmi, Committee Member ; Ruzzene, Massimo, Committee Member ; Smith, Marilyn, Committee Member ; Yu, Yung, Committee Member. Vita. Includes bibliographical references.

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10

Beck, Stephen. "Full-Scale Tilt Rotor Download Reduction." Thesis, The University of Arizona, 2013. http://hdl.handle.net/10150/293744.

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A large-scale model of a tiltrotor wing and flap was built and tested to determine how the size and spacing of fluidic actuators for active flow control should be scaled up from laboratory size models to aircraft size. Flow control was provided by sweeping jet actuators mounted in the flap follower. Chordwise pressure data was collected through pressure taps located along the model centerline. The maximum flap deflection to which the flow could be attached with actuation was compared to previous experiments on a 10% 3D model. An ideal actuator spacing was found and the momentum coefficient wa

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11

Sauvage, Bastien. "Approximation et adaptation numériques pour les écoulements en machines tournantes." Electronic Thesis or Diss., Université Côte d'Azur, 2024. http://www.theses.fr/2024COAZ5045.

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Ce travail s'inscrit dans un projet de recherche dont l'objectif est de proposer des simulations numériques en fluides (CFD) capables de capturer le bruit produit par les machines tournantes.Cette thèse, au sein de ce projet, à pour objectif d'étudier des méthodes d'adaptation de maillages (instationnaires) pour des écoulements turbulents instationnaires.On commence par décrire les outils nécessaires à nos études, à savoir les méthodes numériques, les modèles de turbulences et l'adaptation de maillages. Une première partie est consacrée à l'étude de l'algorithme d'adaptation de maillage instat

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12

Sirakov, Borislav Todorov 1975. "Effects of upstream unsteady flow conditions on rotor tip leakage flow." Thesis, Massachusetts Institute of Technology, 2001. http://hdl.handle.net/1721.1/82235.

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13

Tang, Wei. "Numerical solutions of unsteady flow past rotor sections." Diss., Georgia Institute of Technology, 1986. http://hdl.handle.net/1853/13336.

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14

Shankare, Gowda Vrishank Raghav. "Radial flow effects on a retreating rotor blade." Diss., Georgia Institute of Technology, 2014. http://hdl.handle.net/1853/53403.

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This work studies the effects of radial flow on the aerodynamic phenomena occurring on a retreating blade with a focus on dynamic stall and reverse flow as applied to both a helicopter rotor in forward flight and a wind turbine operating at a yaw angle. While great progress has been made in understanding the phenomenon of two-dimensional dynamic stall, the effect of rotation on the dynamic stall event is not well understood. Experiments were conducted on a rigid two bladed teetering rotor at high advance ratios in a low speed wind tunnel. Particle image velocimetry (PIV) measurements were used

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15

Mear-Stone, Leah Isobel. "Theoretical modelling of flow in rotor-stator systems." Thesis, University of Bath, 2015. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.681054.

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The prevention of hot gas ingress between rotating and stationary discs in gas turbines is big business, with experimental and computational research being common in the sector. Experimental rigs, operating at a fraction of the engine size and in simulated fluid dynamic conditions, model the engine environment. Computational Fluid Dynamics (CFD) is used in both academia and industry to model the flow and heat transfer in a turbine. CFD is expensive, time consuming and requires detailed experimental validation. The engine designer has a need for simpler, faster mathematical modelling methods, u

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16

Bochette, Nikolaus J. "Computational analysis of flow through a transonic compressor rotor." Thesis, Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2005. http://library.nps.navy.mil/uhtbin/hyperion/05Sep%5FBochette.pdf.

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17

McDarby, John Michael. "Modelling of turbulent rotor-blade flow and ground effect." Thesis, University College London (University of London), 2005. http://discovery.ucl.ac.uk/1444821/.

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Rotor blade flows occur in numerous physical systems from helicopters to fans, and from propellers to food mixers. Many previous studies have concentrated on the laminar flow generated by a set of rotors but in many practical cases the flow is turbulent, a setting in which previous research appears to be mainly experimental or purely numerical. The thesis examines turbulent rotor flow as its prime feature, before moving on to the impact of the ground and side structures on the flow. Whilst there exists a wide variety of rotor blade flows in industry, the present research is motivated by the ap

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18

Lewis, Paul. "Pre-swirl rotor-stator systems : flow and heat transfer." Thesis, University of Bath, 2008. https://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.516951.

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19

Fay, Sarah (Sarah C. ). "The rotor-oscillator flow : searching for coherence amidst chaos." Thesis, Massachusetts Institute of Technology, 2015. http://hdl.handle.net/1721.1/98955.

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Thesis: S.B., Massachusetts Institute of Technology, Department of Mechanical Engineering, 2015.<br>Cataloged from PDF version of thesis.<br>Includes bibliographical references (page 29).<br>Chaotic mixing of highly viscous fluids is common in many biological and industrial processes. This study aims to gain insight about the properties of such common processes by examining one particular case of viscous, chaotic mixing: the rotor-oscillator flow. For some couplings of the rotor motion with its oscillation, this flow has been shown to have coherent islands of fluid parcels surrounded by a sea

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20

Place, James Michael Macgregor. "Three-dimensional flow in core compressors." Thesis, University of Cambridge, 1997. https://www.repository.cam.ac.uk/handle/1810/252313.

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21

Karamolegkos, Konstantinos. "Ducted Tail Rotor Perfomance Prediction Using CFD." Thesis, Cranfield University, 2014. http://dspace.lib.cranfield.ac.uk/handle/1826/9241.

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Aviation industry has a crucial impact on society on the grounds that it offers wider social and economic benefits. The demand of transportation is increasing and it is expected that the worldwide fleet of aircraft and rotorcraft will increase accordingly. This growth will introduce an increased environmental impact which can be controlled with the introduction and the implementation of new and greener technologies which can provide both a reduced carbon foot-print and increased efficiency. Therefore, the simulation of new designs with tools that can capture the flow physics accurately is cruc

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22

Yang, Zhong. "A hybrid flow analysis for rotors in forward flight." Diss., Georgia Institute of Technology, 2000. http://hdl.handle.net/1853/13016.

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23

Zhong, Bowen. "Implicit multi-block Euler/Navier-Stokes simulations for hovering helicopter rotor." Thesis, Cranfield University, 2003. http://dspace.lib.cranfield.ac.uk/handle/1826/10754.

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A three dimensional implicit multiblock Navier-Stokes solver for hovering rotor vortical flow simulations has been developed. The governing equations used are cast in an attached blade rotating frame. Two formulations of the governing equations using the relative or absolute velocity as variables respectively are employed and investigated. The Osher's approximate Riemann solver is used for the convective fluxes evaluation. A modified MUSCL scheme is employed for improving the accuracy of the discretisation for the in viscid fluxes. A Block Incomplete Lower and Upper Decomposition (BILU) is ado

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24

Schmidt, M. J. P. "Blade tip clearance effects on an axial flow compressor rotor." Thesis, Cranfield University, 1985. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.354277.

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25

Roshani, Moghaddam Elham. "Numerical investigation of fluid flow in protruded rotor-stator cavities." Thesis, University of Sussex, 2015. http://sro.sussex.ac.uk/id/eprint/53891/.

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The torque associated with overcoming the losses on a rotating disc is of particular importance to the designers of gas turbine engines. Not only does this represent a reduction in useful work, but it also gives rise to unwanted heating of metal surfaces and the adjacent fluid. This research presents a numerical study on the effect of rotor-mounted bolts on the moment coefficient and flow structure within a rotor–stator cavity under conditions representative of modern gas turbine engine design. Steady-state, two-dimensional and three-dimensional, computational fluid dynamics simulations are ob

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26

Sá, Luís Fernando Nogueira de. "Topology optimization method applied to laminar flow machine rotor design." Universidade de São Paulo, 2016. http://www.teses.usp.br/teses/disponiveis/3/3152/tde-16032017-103709/.

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Flow machines are very important to industry, being widely used on various processes. Performance improvements are relevant factors and can be achieved by using optimization methods, such as topology optimization. Thus, this work aims to develop a method to design radial flow machine rotors operating on laminar regime, by implementing a topology optimization formulation based on density model. The design of a rotor involves firstly modelling the fluid flow by using the Navier-Stokes equations on a rotating reference frame and using the Finite Element Method for solving the differential equatio

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27

Haddow, Colin Richard. "The induced flow through a lifting rotor in forward flight." Thesis, University of Southampton, 1986. https://eprints.soton.ac.uk/52212/.

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A technique has been developed to enable the measurement of the velocity field in the vicinity of a lifting rotor. This involved the use of a triaxial hot-wire probe coupled to a mini-computer. Using this technique extensive flow measurements in one plane (z/R = -0.075) under the rotor were made at advance ratios of 0.1 and 0.067. In addition the rotor thrust, torque and blade bending moments were also measured. The results of the analysis of the time averaged flow show clear evidence that the wake of the rotor rapidly rolls up into 2 `fixed-wing' type vortices. Also indicated is that the valu

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28

Reddy, Urmila Chennuru. "Whole field velocity measurements in three-dimensional periodic flows." Diss., Georgia Institute of Technology, 1999. http://hdl.handle.net/1853/12063.

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29

Boyd, David Douglas Jr. "Rotor/Fuselage Unsteady Interactional Aerodynamics: A New Computational Model." Diss., Virginia Tech, 1999. http://hdl.handle.net/10919/28591.

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A new unsteady rotor/fuselage interactional aerodynamics model has been developed. This model loosely couples a Generalized Dynamic Wake Theory (GDWT) to a Navier-Stokes solution procedure. This coupling is achieved using a newly developed unsteady pressure jump boundary condition in the Navier-Stokes model. The new unsteady pressure jump boundary condition models each rotor blade as a moving pressure jump which travels around the rotor azimuth =and is applied between two adjacent planes in a cylindrical, non-rotating grid. Comparisons are made between predictions using this new model and ex

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30

Quaranta, Erika. "Noise radiation from a ducted rotor in a swirling-translating flow." Thesis, Cranfield University, 2009. http://dspace.lib.cranfield.ac.uk/handle/1826/4577.

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This PhD dissertation investigates the noise radiation produced by a rotor inside a duct, which is convected by a swirling-translating mean flow. The study is based on an extension of Gennaretti's and Morino's boundary element method to the frequency domain for scattering problems in conjunction with a spinning rotor source model in the presence of a swirling-translating flow. Firstly, two different source models of the rotor are analyzed in absence of mean flow. The parametric study of the two dipole components distributed over a ring or a disc shows that the source radius is a crucial par

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31

Arzpeima, Minoo. "CFD Investigation of Flow Structures in Rotor-Stator Disc Cavity Systems." Thesis, KTH, Kraft- och värmeteknologi, 2014. http://urn.kb.se/resolve?urn=urn:nbn:se:kth:diva-153733.

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32

El-Oun, Z. B. "Flow in a shrouded rotor-stator cavity with pre-swirl coolant." Thesis, University of Sussex, 1986. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.379447.

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33

Utomo, Adi Tjipto. "Flow patterns and energy dissipation rates in batch rotor-stator mixers." Thesis, University of Birmingham, 2009. http://etheses.bham.ac.uk//id/eprint/501/.

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The flow pattern and distribution of energy dissipation rate in a batch rotor-stator mixer fitted with disintegrating head have been numerically investigated. Standard k-e turbulence model in conjunction with sliding mesh method was employed and the simulation results were verified by laser Doppler anemometry (LDA) measurements. The agreement between predicted and measured velocity profiles in the bulk and of jet emerging from stator hole was very good. Results showed that the interaction between stator and rotating blades generated periodic fluctuations of jet velocity, flowrate, torque and e

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34

Roberts, Thomas Wesley. "Euler equation computations for the flow over a hovering helicopter rotor." Thesis, Massachusetts Institute of Technology, 1987. http://hdl.handle.net/1721.1/14907.

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Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1987.<br>MICROFICHE COPY AVAILABLE IN ARCHIVES AND AERO.<br>Bibliography: leaves 227-233.<br>by Thomas Wesley Roberts.<br>Ph.D.

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35

Gord, Mahmoud Farzaneh. "Flow and heat transfer in a pre-swirl rotor-stator system." Thesis, University of Bath, 2003. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.288236.

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This thesis describes the computational study of the flow and heat transfer in a directtransfer pre-swirl rotor-stator system. Pre-swirl cooling air enters the system at low radius through angled pre-swirl nozzles, located on the stator, impinges on the rotor and flows outward in the wheel-space between stator and rotor, and leaves the system through receiver holes, located on the rotor. Computations were carried out using a 3D incompressible model, with one discrete pre-swirl nozzle on the stator and cyclic symmetry boundary conditions applied at the tangential faces of the domain. To permit

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36

Daneshmandi, Mohsen. "Self-induced flow circulation by enclosed rotors." Thesis, University of Southampton, 1995. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.261555.

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37

Wang, Juan. "Experimental study of two counter rotating axial flow fans." Thesis, Paris, ENSAM, 2014. http://www.theses.fr/2014ENAM0024/document.

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RESUME : Les machines axiales à rotors contrarotatifs subsoniques sont une bonne solution pour les industries où de fortes élévations de pressions et d'efficacités sont nécessaires sans augmenter le diamètre ou la vitesse de rotation des rotors. Néanmoins, le comportement des CRS et les paramètres impactant ses performances ne sont pas encore totalement compris. Cette thèse mène une investigation expérimentale sur la performance et les paramètres influents sur un étage contrarotatif. La technique de design et les méthodes de mesure sont repris sur une thèse précédente réalisée au laboratoire D

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38

Bellia, J. M. "Aerodynamic measurements on a small HAWT rotor in axial and yawed flow." Thesis, Cranfield University, 1990. http://hdl.handle.net/1826/4290.

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Current wind turbine performance codes are not yet able to predict the rotor aerodynamic behaviour with sufficient certainty. This has led to both the over-design of blades and to operational restrictions in certain wind conditions. Essentially the problem is one of aerodynamic stall. Steady 3-dimensional stall can occur near the blade root in high wind conditions and may produce more power than predicted. Dynamic stall can also be expected due to the effects of yawed operation, turbulence, tower shadow and the earth's boundary layer. The main aim of this work is to provide a coherent set of m

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39

Li, Yiguang. "Three-Dimensional Flow and Performance Simulation of Multistage Axial Flow Compressors." Thesis, Cranfield University, 2000. http://dspace.lib.cranfield.ac.uk/handle/1826/4591.

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\Yith the current develop111ent in computer technology and Computational Fluid D)"n<'tlllics techniques, t.he si11utlation within axial flow compressors becomes 1110re and 1110re pract.ical and beneficial to the compressor designs. Due to the insufficient capabilit)" of today's COll1put.ers for three-dimensional unsteady flow 1110delling of 111Ult i~Llg(' axial flow compressors, sophisticated models of steady state flow and perfor111ance 1110delling of the C0111prcssors deserve to be thoroughly investigated. In l1utltistage C0111pressor sinlulations with steady state methods, frame of referenc

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40

Frohnapfel, Dustin Joseph. "Experimental Investigation of Fan Rotor Response to Inlet Swirl Distortion." Thesis, Virginia Tech, 2016. http://hdl.handle.net/10919/71323.

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Next generation aircraft design focuses on highly integrated airframe/engine architectures that exploit advantages in system level efficiency and performance. One such design concept incorporates boundary layer ingestion which locates the turbofan engine inlet near enough to the lifting surface of the aircraft skin that the boundary layer is ingested and reenergized. This process reduces overall aircraft drag and associated required thrust, resulting in fuel savings and decreased emissions; however, boundary layer ingestion also creates unique challenges for the turbofan engines operating in

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41

Lal, Mihir Kumar. "Unsteady pressure and inflow velocity on a pitching rotor blade in hover." Diss., Georgia Institute of Technology, 1993. http://hdl.handle.net/1853/12053.

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42

Mischo, Bob. "Axial turbine rotor aero-thermal blade tip performance improvement through flow control /." Zürich : ETH, 2008. http://e-collection.ethbib.ethz.ch/show?type=diss&nr=17813.

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43

Smitley, Eric D. "Development of a cross-flow fan powered quad-rotor unmanned aerial vehicle." Thesis, Monterey, California: Naval Postgraduate School, 2015. http://hdl.handle.net/10945/45946.

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Approved for public release; distribution is unlimited<br>The research presented is dedicated to the advancement of construction techniques in order to implement new designs of a vehicle suited for cross-flow fan propulsion. This is accomplished by designing a quad-rotor cross-flow fan that incorporates lessons learned from previous generation models as well introducing novel new construction concepts tailored to cross-flow fan propulsion vehicles. The current vehicle design was built using both custom and standard sections. Commercially available drivetrain and control components are used. Th

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44

Karabay, Hasan. "Flow and heat transfer in cover-plate pre-swirl rotor-stator system." Thesis, University of Bath, 1998. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.242797.

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45

Van, der Spuy Sybrand Johannes. "The design of a low-noise rotor-only axial flow fan series." Thesis, Stellenbosch : University of Stellenbosch, 1997. http://hdl.handle.net/10019.1/20977.

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ENGLISH ABSTRACT: A design routine was derived for designing a series of rotor-only axial flow fans. The routine was applied by designing two different series of axial flow fans. The first design was for a general application rotor-only axial flow fan. This fan series was designed, built and tested in co-operation with Howden Air Industries for both research and commercial purposes. The second design was for a low-noise fan series, which was designed, built and tested by the University of Stellenbosch for research purposes only. The design theory used the principle of blade cropping, me

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46

Brown, Kieron David. "Computational analysis of low speed axial flow rotors." Thesis, University of Bristol, 1998. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.389158.

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47

Morris, Mary Beth. "Flow randomness and tip losses in transonic rotors." Thesis, This resource online, 1992. http://scholar.lib.vt.edu/theses/available/etd-07212009-040241/.

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48

Pan, Shunqi. "An experimental study of swirl development along the annulus between a rotor and a stator." Thesis, Heriot-Watt University, 1993. http://hdl.handle.net/10399/1407.

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49

Couch, Mark A. "A three-dimensional flutter theory for rotor blades with trailing-edge flaps." Monterey, Calif. : Springfield, Va. : Naval Postgraduate School ; Available from National Technical Information Service, 2003. http://library.nps.navy.mil/uhtbin/hyperion-image/03Jun%5fCouch%5FPhD.pdf.

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Thesis (Ph. D. in Aeronautical and Astronautical Engineering)--Naval Postgraduate School, June 2003.<br>Dissertation supervisor and advisor: E. Roberts Wood. Includes bibliographical references (p. 205-210). Also available online.

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50

Akers, Walter John. "Flourescent molecular rotors as mechanosensors in biofluids." Diss., Columbia, Mo. : University of Missouri-Columbia, 2005. http://hdl.handle.net/10355/4114.

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Abstract:

Thesis (Ph. D.)--University of Missouri-Columbia, 2005.<br>The entire dissertation/thesis text is included in the research.pdf file; the official abstract appears in the short.pdf file (which also appears in the research.pdf); a non-technical general description, or public abstract, appears in the public.pdf file. Title from title screen of research.pdf file (viewed on October 19, 2007) Vita. Includes bibliographical references.

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