Log in

Relevant bibliographies by topics / Boundary layer turbine / Books

To see the other types of publications on this topic, follow the link: Boundary layer turbine.

Books on the topic 'Boundary layer turbine'

Author: Grafiati

Published: 4 June 2021

Last updated: 9 March 2023

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

Select a source type:

Consult the top 31 books for your research on the topic 'Boundary layer 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 books on a wide variety of disciplines and organise your bibliography correctly.

1

Abdul-Aziz, Ali. Thermal finite-element analysis of space shutle main engine turbine blade. National Aeronautics and Space Administration, Lewis Research Center, 1987.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

2

T, Tong Michael, Kaufman Albert 1928-, and Lewis Research Center, eds. Thermal finite-element analysis of space shutle main engine turbine blade. National Aeronautics and Space Administration, Lewis Research Center, 1987.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

3

Abdul-Aziz, Ali. Thermal finite-element analysis of space shutle main engine turbine blade. National Aeronautics and Space Administration, Lewis Research Center, 1987.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

4

B, Caplin, and United States. National Aeronautics and Space Administration., eds. User's manual for three dimensional boundary layer (BL3-D) code. United Technologies Research Center, 1985.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

5

Center, Lewis Research, ed. Experimental study of boundary layer behavior in a simulated low pressure turbine. National Aeronautics and Space Administration, Lewis Research Center, 1998.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

6

Center, Lewis Research, ed. Experimental study of boundary layer behavior in a simulated low pressure turbine. National Aeronautics and Space Administration, Lewis Research Center, 1998.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

7

J, Dorney Daniel, and Lewis Research Center, eds. Study of boundary layer development in a two-stage low-pressure turbine. National Aeronautics and Space Administration, Lewis Research Center, 1999.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

8

Schmidt, Rodney C. Two-equation low-Reynolds-number turbulence modeling of transitional boundary layer flows characteristic of gas turbine blades. Lewis Research Center, 1988.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

9

Ameri, A. A. Analysis of gas turbine rotor blade tip and shroud heat transfer. National Aeronautics and Space Administration, 1996.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

10

Ameri, A. A. Analysis of gas turbine rotor blade tip and shroud heat transfer. National Aeronautics and Space Administration, 1998.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

11

United States. National Aeronautics and Space Administration., ed. Assessment of a 3-D boundary layer analysis to predict heat transfer and flow field in a turbine passage. United Technologies Research Center, 1985.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

12

Lakshminarayana, B. The three dimensional flow field at the exit of an axial-flow turbine rotor. National Aeronautics and Space Administration, Lewis Research Center, 1998.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

13

Lakshminarayana, B. The three dimensional flow field at the exit of an axial-flow turbine rotor. National Aeronautics and Space Administration, Lewis Research Center, 1998.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

14

Corke, Thomas C. Enhanced design of turbo-jet LPT by separation control using phased plasma actuators. National Aeronautics and Space Administration, Glenn Research Center, 2003.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

15

Corke, Thomas C. Enhanced design of turbo-jet LPT by separation control using phased plasma actuators. National Aeronautics and Space Administration, Glenn Research Center, 2003.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

16

Corke, Thomas C. Enhanced design of turbo-jet LPT by separation control using phased plasma actuators. National Aeronautics and Space Administration, Glenn Research Center, 2003.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

17

Center, Lewis Research, ed. Transition in turbines: Proceedings of a symposium held at NASA Lewis Research Center, Cleveland, Ohio, May 15-16, 1984. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

18

Williams, Warren W. Effects of an embedded vortex on a single film-cooling jet in a turbulent boundary layer. Naval Postgraduate School, 1988.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

19

P, Shreeve Raymond, and Lewis Research Center, eds. Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading. National Aeronautics and Space Administration, Lewis Research Center, 1986.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

20

Thermal finite-element analysis of space shutle main engine turbine blade. National Aeronautics and Space Administration, Lewis Research Center, 1987.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

21

National Aeronautics and Space Administration (NASA) Staff. Study of Boundary Layer Development in a Two-Stage Low-Pressure Turbine. Independently Published, 2018.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

22

Boundary-Layer Breakthrough (The Bladeless Tesla Turbine, Volume II: Tesla Technology Series). High Energy Enterprises, 1990.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

23

Two-equation low-Reynolds-number turbulence modeling of transitional boundary layer flows characteristic of gas turbine blades. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

24

Two-equation low-Reynolds-number turbulence modeling of transitional boundary layer flows characteristic of gas turbine blades. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

25

Use of Dimples to Suppress Boundary Layer Separation on a Low Pressure Turbine Blade. Storming Media, 2002.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

26

Mach number effects on turbine blade transition length prediction. National Aeronautics and Space Administration, Lewis Research Center, 1998.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

27

Effect of Dimple Pattern on the Suppression of Boundary Layer Separation on a Low Pressure Turbine Blade. Storming Media, 2004.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

28

Assessment of a 3-D boundary layer analysis to predict heat transfer and flow field in a turbine passage. United Technologies Research Center, 1985.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

29

Transition in turbines: Proceedings of a symposium held at NASA Lewis Research Center, Cleveland, Ohio, May 15-16, 1984. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Find full text

APA, Harvard, Vancouver, ISO, and other styles

30

Escudier, Marcel. Introduction to Engineering Fluid Mechanics. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.001.0001.

Full text

Abstract:

Turbojet and turbofan engines, rocket motors, road vehicles, aircraft, pumps, compressors, and turbines are examples of machines which require a knowledge of fluid mechanics for their design. The aim of this undergraduate-level textbook is to introduce the physical concepts and conservation laws which underlie the subject of fluid mechanics and show how they can be applied to practical engineering problems. The first ten chapters are concerned with fluid properties, dimensional analysis, the pressure variation in a fluid at rest (hydrostatics) and the associated forces on submerged surfaces, the relationship between pressure and velocity in the absence of viscosity, and fluid flow through straight pipes and bends. The examples used to illustrate the application of this introductory material include the calculation of rocket-motor thrust, jet-engine thrust, the reaction force required to restrain a pipe bend or junction, and the power generated by a hydraulic turbine. Compressible-gas flow is then dealt with, including flow through nozzles, normal and oblique shock waves, centred expansion fans, pipe flow with friction or wall heating, and flow through axial-flow turbomachinery blading. The fundamental Navier-Stokes equations are then derived from first principles, and examples given of their application to pipe and channel flows and to boundary layers. The final chapter is concerned with turbulent flow. Throughout the book the importance of dimensions and dimensional analysis is stressed. A historical perspective is provided by an appendix which gives brief biographical information about those engineers and scientists whose names are associated with key developments in fluid mechanics.

APA, Harvard, Vancouver, ISO, and other styles

31

Aerodynamics and heat transfer investigations on a high Reynolds number turbine cascade. NASA, 1991.

Find 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!