Log in

Relevant bibliographies by topics / Jet Turbine / Dissertations / Theses

To see the other types of publications on this topic, follow the link: Jet Turbine.

Dissertations / Theses on the topic 'Jet Turbine'

Author: Grafiati

Published: 4 June 2021

Last updated: 5 May 2022

Create a spot-on reference in APA, MLA, Chicago, Harvard, and other styles

Select a source type:

Consult the top 50 dissertations / theses for your research on the topic 'Jet Turbine.'

Next to every source in the list of references, there is an 'Add to bibliography' button. Press on it, and we will generate automatically the bibliographic reference to the chosen work in the citation style you need: APA, MLA, Harvard, Chicago, Vancouver, etc.

You can also download the full text of the academic publication as pdf and read online its abstract whenever available in the metadata.

Browse dissertations / theses on a wide variety of disciplines and organise your bibliography correctly.

1

Goodisman, Michael I. "Turbine turbobrake systems." Thesis, University of Oxford, 1991. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.305994.

Full text

APA, Harvard, Vancouver, ISO, and other styles

2

Tapanlis, Orpheas. "Turbine casing impingement cooling systems." Thesis, University of Oxford, 2011. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.711623.

Full text

APA, Harvard, Vancouver, ISO, and other styles

3

Abdul, Aziz M. M. "Liquid fuelled jet shear layer gas turbine combustion." Thesis, University of Leeds, 1988. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.233835.

Full text

APA, Harvard, Vancouver, ISO, and other styles

4

Andrews, G. E. "Gas turbine combustion with low emissions." Thesis, University of Leeds, 1989. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.329381.

Full text

APA, Harvard, Vancouver, ISO, and other styles

5

Brookes, S. J. "Soot Production and Thermal Radiation from Turbulent Jet Diffusion Flames." Thesis, Cranfield University, 1996. http://hdl.handle.net/1826/3558.

Full text

Abstract:

The aim of this study is to advance the present capability for modelling soot production and thermal radiation from turbulent jet diffusion flames. Turbulent methane / air jet diffusion flames at atmospheric and elevated pressure are studied experimentally to provide data for subsequent model development and validation. Methane is only lightly sooting at atmospheric pressure whereas at elevated pressure the soot yield increases greatly. This allows the creation of an optically thick, highly radiating flame within a laboratory scale rig. Essential flame properties needed for model validation ar

APA, Harvard, Vancouver, ISO, and other styles

6

Ebaid, Munzer Shehadeh Yousef. "Design and construction of a small gas turbine to drive a permanent magnet high speed generator." Thesis, University of Hertfordshire, 2002. http://hdl.handle.net/2299/14046.

Full text

Abstract:

Radial gas turbines engines have established prominence in the field of small turbomachinery because of their simplicity, relatively high performance and installation features. Thus they have been used in a variety of applications such as generator sets, small auxiliary power units (APu), air conditioning of aircraft cabins and hybrid electric vehicles turbines. The current research describes the design, manufacturing, construction and testing a radial type small gas turbine. The aim was to design and build the engine to drive directly a high-speed permanent magnet alternator running at 60000

APA, Harvard, Vancouver, ISO, and other styles

7

Spencer, A. "Gas turbine combustor port flows." Thesis, Loughborough University, 1998. https://dspace.lboro.ac.uk/2134/6883.

Full text

Abstract:

Competitive pressure and stringent emissions legislation have placed an urgent demand on research to improve our understanding of the gas turbine combustor flow field. Flow through the air admission ports of a combustor plays an essential role in determining the internal flow patterns on which many features of combustor performance depend. This thesis explains how a combination of experimental and computational research has helped improve our understanding, and ability to predict, the flow characteristics of jets entering a combustor. The experiments focused on a simplified generic geometry of

APA, Harvard, Vancouver, ISO, and other styles

8

Ahmad, N. T. "Swirl stabilised gas turbine combustion." Thesis, University of Leeds, 1986. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.356423.

Full text

APA, Harvard, Vancouver, ISO, and other styles

9

White, Alexander John. "Condensation in steam turbine cascades." Thesis, University of Cambridge, 1992. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.259523.

Full text

APA, Harvard, Vancouver, ISO, and other styles

10

Sudol, Eugene G. "Evaluation of aircraft turbine redesigns." Monterey, California : Naval Postgraduate School, 1990. http://handle.dtic.mil/100.2/ADA237599.

Full text

Abstract:

Thesis (M.S. in Management)--Naval Postgraduate School, June 1990.<br>Thesis Advisor(s): Carrick, Paul M. Second Reader: Doyle, Richard B. "June 1990." Description based on title screen as viewed on October 16, 2009. DTIC Identifier(s): Jet Engines, Engine Components, Cost Analysis, Gas Turbines, Optimizations, Naval Logistics, Aircraft Maintenance, CIP(Component Improvement Program), Benefits, Redesign, Naval Aircraft, Mean Time Between Failure, Data Bases, Theses. Author(s) subject terms: Aircraft Turbine Engine Redesigns Component Improvement Program. Includes bibliographical references (p.

APA, Harvard, Vancouver, ISO, and other styles

11

Ismail, Ibrahim H. "Simulation of aircraft gas turbine engine." Thesis, University of Hertfordshire, 1991. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.303465.

Full text

APA, Harvard, Vancouver, ISO, and other styles

12

Abdul, Husein Reyad Abdul Ameer. "Impingement cooling of gas turbine components." Thesis, University of Leeds, 1990. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.255236.

Full text

APA, Harvard, Vancouver, ISO, and other styles

13

Zedda, M. "Gas turbine engine and sensor fault diagnosis." Thesis, Cranfield University, 1999. http://dspace.lib.cranfield.ac.uk/handle/1826/9117.

Full text

Abstract:

Substantial economic and even safety related gains can be achieved if effective gas turbine performance analysis is attained. During the development phase, analysis can help understand the effect on the various components and on the overall engine performance of the modifications applied. During usage, analysis plays a major role in the assessment of the health status of the engine. Both condition monitoring of operating engines and pass off tests heavily rely on the analysis. In spite of its relevance, accurate performance analysis is still difficult to achieve. A major cause of this is measu

APA, Harvard, Vancouver, ISO, and other styles

14

Huntsman, Ian. "An investigation of radial inflow turbine aerodynamics." Thesis, University of Cambridge, 1993. https://www.repository.cam.ac.uk/handle/1810/251556.

Full text

APA, Harvard, Vancouver, ISO, and other styles

15

Duncan, John Robert. "The analysis and improvement of the overall and component performance of a small jet engine." Thesis, Queen's University Belfast, 1986. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.328168.

Full text

APA, Harvard, Vancouver, ISO, and other styles

16

Harrison, Stephen. "The influence of blade stacking on turbine losses." Thesis, University of Cambridge, 1989. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.333326.

Full text

APA, Harvard, Vancouver, ISO, and other styles

17

Day, Charles. "Aerodynamics of an annular film-cooled turbine cascade." Thesis, University of Oxford, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.362028.

Full text

APA, Harvard, Vancouver, ISO, and other styles

18

Thompson, Haydn Ashley. "Parallel processing applications for gas turbine engine control." Thesis, Bangor University, 1990. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.254683.

Full text

APA, Harvard, Vancouver, ISO, and other styles

19

MacCallum, N. R. L. "Studies in gas turbine performance and in combustion." Thesis, University of Glasgow, 2000. http://theses.gla.ac.uk/5335/.

Full text

APA, Harvard, Vancouver, ISO, and other styles

20

Biesinger, Thomas Ernst. "Secondary flow reduction techniques in linear turbine cascades." Thesis, Durham University, 1993. http://etheses.dur.ac.uk/5626/.

Full text

Abstract:

This thesis investigates a novel secondary flow reduction method. The inlet boundary layer to a linear turbine cascade is skewed by injection of air through an upstream slot to oppose regular generated negative stream wise vorticity. Other methods from the pertinent literature are reviewed on a broad basis. Detailed measurements of the flowfield in the Durham Linear Cascade facility have shown that substantial reductions in secondary flows and losses are possible. If the kinetic energy required for the blowing is taken into account by means of an availability analysis, no net gain in loss is a

APA, Harvard, Vancouver, ISO, and other styles

21

Da, Palma Jose Manuel Laginha Mestre. "Mixing in non-reacting gas turbine combustor flows." Thesis, Imperial College London, 1989. http://hdl.handle.net/10044/1/47606.

Full text

APA, Harvard, Vancouver, ISO, and other styles

22

Koutmos, P. "An isothermal study of gas turbine combustor flows." Thesis, Imperial College London, 1985. http://hdl.handle.net/10044/1/37748.

Full text

APA, Harvard, Vancouver, ISO, and other styles

23

Stuttaford, Peter J. "Preliminary gas turbine combustor design using a network approach." Thesis, Cranfield University, 1997. http://hdl.handle.net/1826/1038.

Full text

Abstract:

Gas turbine combustor design represents an ambitious task in numerical and experimental analysis. A significant number of competing criteria must be optimised within specified constraints in order to satisfy legislative and performance requirements. Currently, preliminary combustor flow and heat transfer design procedures, which by necessity involve semi-empirical models, are often restricted in their range of application. The objective of this work is the development of a versatile design tool able to model all conceivable gas turbine combustor types. A network approach provides the foundatio

APA, Harvard, Vancouver, ISO, and other styles

24

Provost, M. J. "The use of optimal estimation techniques in the analysis of gas turbines." Thesis, Cranfield University, 1994. http://hdl.handle.net/1826/2703.

Full text

Abstract:

This thesis discusses several methods that can be used to analyse gas turbines, based on an optimal estimation algorithm called the Kalman Filter. These techniques overcome the difficulties of more 'traditional' analysis methods, which can give misleading results because they do not explicitly consider the possibility of measurement error. An enhancement to the Kalman Filter (the 'Concentrator') is presented, which overcomes the Kalman Filter's tendency to 'smear' the effects of genuine changes in a small number of component changes and/or sensor biasses over the whole set of changes and bias

APA, Harvard, Vancouver, ISO, and other styles

25

Lyes, Peter A. "Low speed axial compressor design and evaluation : High speed representation and endwall flow control studies." Thesis, Cranfield University, 1999. http://hdl.handle.net/1826/4251.

Full text

Abstract:

This Thesis reports the design, build and test of two sets of blading for the Cranfield University low speed research compressor. The first of these was a datum low speed design based on the fourth stage of the DERA high speed research compressor C 147. The emphasis of this datum design was on the high-to-low speed transformation process and the evaluation of such a process through comparing detailed flow measurements from both compressors. Area traverse measurements in both the stationary and rotating frame of reference were taken at Cranfield along with overall performance, blade surface sta

APA, Harvard, Vancouver, ISO, and other styles

26

Churchhouse, Stephen Paul. "Multivariable control of a propfan engine." Thesis, University of Cambridge, 1988. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.303222.

Full text

APA, Harvard, Vancouver, ISO, and other styles

27

Duta, Mihai C. "The use of the adjoint method for the minimisation of forced vibration in turbomachinery." Thesis, University of Oxford, 2002. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.249540.

Full text

APA, Harvard, Vancouver, ISO, and other styles

28

Chen, Lihong. "Numerical and experimental modelling of brush seals." Thesis, University of Oxford, 1998. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.268200.

Full text

APA, Harvard, Vancouver, ISO, and other styles

29

Abu, Talib Abd Rahim. "Detailed investigation of the low-temperature analogy of an aircraft engine standard fire-test." Thesis, University of Oxford, 2003. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.289368.

Full text

APA, Harvard, Vancouver, ISO, and other styles

30

Neal, P. M. "Data acquisition for turbomachinery (MORDAS)." Thesis, University of Oxford, 1994. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.282719.

Full text

APA, Harvard, Vancouver, ISO, and other styles

31

Smith, Warren Robert. "High velocity gas journal bearings." Thesis, University of Oxford, 1992. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.317910.

Full text

APA, Harvard, Vancouver, ISO, and other styles

32

Sheldrake, C. D. "Unsteady effects in the high pressure stage of a model gas turbine." Thesis, University of Oxford, 1995. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.242794.

Full text

APA, Harvard, Vancouver, ISO, and other styles

33

Wang, Zuolan. "The application of thermochromic liquid crystals to detailed turbine blade cooling measurements." Thesis, University of Oxford, 1991. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.303677.

Full text

APA, Harvard, Vancouver, ISO, and other styles

34

Hancock, Simon David. "Gas turbine engine controller design using multi-objective optimization techniques." Thesis, Bangor University, 1992. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.304616.

Full text

APA, Harvard, Vancouver, ISO, and other styles

35

Pradeepkumar, K. N. "Analysis of a 115MW, 3 shaft, helium Brayton cycle." Thesis, Cranfield University, 2002. http://dspace.lib.cranfield.ac.uk/handle/1826/9219.

Full text

Abstract:

This research theme is originated from a development project that is going on in South Africa, for the design and construction of a closed cycle gas turbine plant using gas-cooled reactor as the heat source to generate 115 MW of electricity. South African Power utility company, Eskom, promotes this developmental work through its subsidiary called PBMR (Pebble Bed Modular Reactor). Some of the attractive features of this plant are the inherent and passive safety features, modular geometry, small evacuation area, small infrastructure requirements for the installation and running of the plant, sm

APA, Harvard, Vancouver, ISO, and other styles

36

Wang, Xu. "A study into vibrations of turbocharger blading with a lacing wire." Thesis, Loughborough University, 1994. https://dspace.lboro.ac.uk/2134/10754.

Full text

Abstract:

The vibration of a turbocharger blade and dynamic characteristics of bladed packets connected by a lacing wire have been studied. The study was carried out using three analytical and experimental methods. They are: Modal Testing, Electronic Speckle Pattern Interferometry (ESPD and Finite Element Analysis (FEA)). Vibration modes of a turbocharger blade with aerodynamic profile, with and without a lacing wire, were identified using model blades with simplified geometry. The separation of coupled modes was achieved using ESPI tests. The modes of vibrations of bladed packets were identified. The e

APA, Harvard, Vancouver, ISO, and other styles

37

Chen, Hua. "Steady and unsteady performance of vaneless casing radial-inflow turbines." Thesis, University of Manchester, 1990. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.291004.

Full text

APA, Harvard, Vancouver, ISO, and other styles

38

Abdullah, Abu Hasan. "The application of high inlet swirl angles for broad operating range turbocharger compressor." Thesis, University of Bath, 1996. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.320555.

Full text

APA, Harvard, Vancouver, ISO, and other styles

39

Mahmoud, Saad M. "Effective optimal control of a fighter aircraft engine." Thesis, Loughborough University, 1988. https://dspace.lboro.ac.uk/2134/7287.

Full text

Abstract:

Typical modem fighter aircraft use two-spool, low by-pass ratio, turbojet engines to provide the thrust needed to carry out the combat manoeuvres required by present-day air warfare tactics. The dynamic characteristics of such aircraft engines are complex and non-linear. The need for fast, accurate control of the engine throughout the flight envelope is of paramount importance and this research was concerned with the study of such problems and subsequent design of an optimal linear control which would improve the engine's dynamic response and provide the required correspondence between the out

APA, Harvard, Vancouver, ISO, and other styles

40

Chen, Rui. "Fluidic devices as fuel injectors for natural gas engines." Thesis, Loughborough University, 1997. https://dspace.lboro.ac.uk/2134/13566.

Full text

Abstract:

A novel, fast switching, reliable, and economical fluidic gaseous fuel injector system designed for natural gas engines has been developed in this research. The system consists mainly of no-moving-part fluidic devices and piezo-electric controlling interfaces. The geometric parameters of a fluidic device seriously affect its performance. Traditionally, these parameters can only be optimised through "trial and error" exercise. In this research, a computer simulation model for the jet steady state attachment and dynamic switching has been developed. The good agreements between predicted results

APA, Harvard, Vancouver, ISO, and other styles

41

Vasanthakumar, Parthasarathy. "Three dimensional frequency-domain solution method for unsteady turbomachinery flows." Thesis, Durham University, 2003. http://etheses.dur.ac.uk/3089/.

Full text

Abstract:

The three-dimensional calculation of unsteady flows is increasingly gaining importance in the prediction of turbomachinery flow problems. A three-dimensional Euler/Navier-Stokes solver incorporating the time-linearized method and the nonlinear harmonic method in the frequency domain has been developed for predicting unsteady turbomachinery flows. In the time-linearized method, the flow is decomposed into a steady part and a harmonic perturbation part. Linearization results in a steady flow equation and a time-linearized perturbation equation. A pseudo-time time-marching technique is introduced

APA, Harvard, Vancouver, ISO, and other styles

42

Mahon, Patrick Gerard. "Development of a testing facility for verification of radial turbine design procedures and off-design performance predictions." Thesis, Queen's University Belfast, 1991. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.334483.

Full text

APA, Harvard, Vancouver, ISO, and other styles

43

McDonnell, Gavin Thomas. "The design, development and testing of a turbine hydraulic dynamometer." Thesis, Queen's University Belfast, 1999. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.287447.

Full text

APA, Harvard, Vancouver, ISO, and other styles

44

Farrell, Brian Henry. "An experimental and theoretical investigation into simple, low cost combustion chambers for small gas turbines." Thesis, Queen's University Belfast, 1989. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.335334.

Full text

APA, Harvard, Vancouver, ISO, and other styles

45

Farrall, Mark. "Numerical modelling of two-phase flow in a simplified bearing chamber." Thesis, University of Nottingham, 2000. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.367991.

Full text

APA, Harvard, Vancouver, ISO, and other styles

46

Boumedmed, Abdelkader. "The use of variable engine geometry to improve the transient performance of a two-spool turbofan engine." Thesis, University of Glasgow, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.263451.

Full text

APA, Harvard, Vancouver, ISO, and other styles

47

Ji, Chunjun. "Vortex cloud method and its applications to turbomachine cascades." Thesis, University of Newcastle Upon Tyne, 1997. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.360327.

Full text

APA, Harvard, Vancouver, ISO, and other styles

48

Patel, Vijaykumar Chhaganlal. "Modelling and intelligent fault detection and isolation of aero gas turbine engines." Thesis, University of Sheffield, 1998. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.286615.

Full text

APA, Harvard, Vancouver, ISO, and other styles

49

Neilson, Richard David. "Dynamics of simple rotor systems having motion dependent discontinuities." Thesis, University of Dundee, 1986. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.362927.

Full text

APA, Harvard, Vancouver, ISO, and other styles

50

Taylor, Mark David. "An investigation into the gas dynamics of an aerovalve pulsejet engine for acoustic aerosol scavenging." Thesis, University of Strathclyde, 2003. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.273427.

Full text

APA, Harvard, Vancouver, ISO, and other styles

We offer discounts on all premium plans for authors whose works are included in thematic literature selections. Contact us to get a unique promo code!