A Numerical and Experimental Investigation of Two-dimensional Compressible Turbine Tip Gap Flow

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Total Pages : pages
Book Rating : 4.:/5 (535 download)

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Book Synopsis A Numerical and Experimental Investigation of Two-dimensional Compressible Turbine Tip Gap Flow by : Guangli Chen Fordham

Download or read book A Numerical and Experimental Investigation of Two-dimensional Compressible Turbine Tip Gap Flow written by Guangli Chen Fordham and published by . This book was released on 1994 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Numerical and Experimental Investigation of Turbine Tip Gap Flow

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis A Numerical and Experimental Investigation of Turbine Tip Gap Flow by : G. Chen

Download or read book A Numerical and Experimental Investigation of Turbine Tip Gap Flow written by G. Chen and published by . This book was released on 1993 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Theoretical and Experimental Investigation of Two-dimensional Effects on Unsteady Flow in a Partial Admission Turbine

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ISBN 13 :
Total Pages : 264 pages
Book Rating : 4.:/5 (255 download)

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Book Synopsis A Theoretical and Experimental Investigation of Two-dimensional Effects on Unsteady Flow in a Partial Admission Turbine by : Kuo-Hua Chu

Download or read book A Theoretical and Experimental Investigation of Two-dimensional Effects on Unsteady Flow in a Partial Admission Turbine written by Kuo-Hua Chu and published by . This book was released on 1966 with total page 264 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 704 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 704 pages. Available in PDF, EPUB and Kindle. Book excerpt:

93-2250 - 93-2299

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ISBN 13 :
Total Pages : 580 pages
Book Rating : 4.0/5 ( download)

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Book Synopsis 93-2250 - 93-2299 by :

Download or read book 93-2250 - 93-2299 written by and published by . This book was released on 1992 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Analysis of two-dimensional turbine cascade flow by finite area method

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ISBN 13 :
Total Pages : 15 pages
Book Rating : 4.:/5 (946 download)

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Book Synopsis Analysis of two-dimensional turbine cascade flow by finite area method by :

Download or read book Analysis of two-dimensional turbine cascade flow by finite area method written by and published by . This book was released on 1985 with total page 15 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of Partial- and Full-admission Characteristics of a Two-stage Velocity-compounded Turbine

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ISBN 13 :
Total Pages : 26 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Experimental Investigation of Partial- and Full-admission Characteristics of a Two-stage Velocity-compounded Turbine by : Thomas P. Moffitt

Download or read book Experimental Investigation of Partial- and Full-admission Characteristics of a Two-stage Velocity-compounded Turbine written by Thomas P. Moffitt and published by . This book was released on 1960 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

International Aerospace Abstracts

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ISBN 13 :
Total Pages : 980 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis International Aerospace Abstracts by :

Download or read book International Aerospace Abstracts written by and published by . This book was released on 1998 with total page 980 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Numerical and experimental investigation of the wake flow downstream of a linear turbine cascade, ASME 98-GT-246

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ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (137 download)

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Book Synopsis Numerical and experimental investigation of the wake flow downstream of a linear turbine cascade, ASME 98-GT-246 by : Wolfgang Sanz

Download or read book Numerical and experimental investigation of the wake flow downstream of a linear turbine cascade, ASME 98-GT-246 written by Wolfgang Sanz and published by . This book was released on 1998 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: Presented at the International Gas Turbine & Aeroengine Congress & Exhibition, Stockholm, Sweden, June 2 - June 5, 1998.

An Experimental Investigation Into The Two-dimensional Turbulent Flow In 90 Degree Duct Bends

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ISBN 13 :
Total Pages : 286 pages
Book Rating : 4.:/5 (775 download)

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Book Synopsis An Experimental Investigation Into The Two-dimensional Turbulent Flow In 90 Degree Duct Bends by : Donald Gillard

Download or read book An Experimental Investigation Into The Two-dimensional Turbulent Flow In 90 Degree Duct Bends written by Donald Gillard and published by . This book was released on 1965 with total page 286 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Some Features of Tip Gap Flow Fields of a Linear Compressor Cascade

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Total Pages : 0 pages
Book Rating : 4.:/5 (946 download)

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Book Synopsis Some Features of Tip Gap Flow Fields of a Linear Compressor Cascade by :

Download or read book Some Features of Tip Gap Flow Fields of a Linear Compressor Cascade written by and published by . This book was released on 2003 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This report presents results from an experimental study of three-dimensional turbulent tip gap flows in the linear cascade wind tunnel for two different tip gap clearances (t/c=1.65% and 3.3%). Three experimental techniques are used to measure the tip gap velocity field and static pressure field on the end-wall: a three-orthogonal-velocity-component fiber-optic laser Doppler anemometer (3D-LDA) system, surface oil flow visualization and a scani-valve pressure measurement system. The end-wall skin friction velocity is calculated from near-wall LDA data and pressure gradient data using the near-wall momentum equation. The statistics of Reynolds stresses and triple products in the two-dimensional turbulent boundary layer and three-dimensional turbulent boundary layer were examined using a velocity fluctuation octant analysis. The octant analysis for the two-dimensional turbulent boundary layer reveals that ejections and sweeps are the dominant coherent motions. The octant analysis for the three-dimensional turbulent boundary layer in the tip gap shows that the dominant octant events are partially different from those in the two-dimensional turbulent boundary layer, but ejections and sweeps are still the dominant coherent motions. For the three-dimensional turbulent boundary layer in the moving wall flow, the near-wall shear flow reinforces the sweep motion to the moving wall and weakens the outward ejection motion in the shear flow dominant region. Between the passage flow and the shear flow is the interaction region of the high speed streaks and the low speed streaks. This is the first time that the coherent structure of the three-dimensional turbulent boundary in the linear cascade tip gap has been studied.

Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 300)

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ISBN 13 :
Total Pages : 686 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 300) by :

Download or read book Aeronautical Engineering: A Cumulative Index to a Continuing Bibliography (supplement 300) written by and published by . This book was released on 1994 with total page 686 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of the Three-dimensional Flow and Losses in an Axial Flow Turbine Stage

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ISBN 13 :
Total Pages : 12 pages
Book Rating : 4.:/5 (187 download)

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Book Synopsis Experimental Investigation of the Three-dimensional Flow and Losses in an Axial Flow Turbine Stage by : Ning Wei

Download or read book Experimental Investigation of the Three-dimensional Flow and Losses in an Axial Flow Turbine Stage written by Ning Wei and published by . This book was released on 1992 with total page 12 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Numerical and Experimental Investigation of Flow in Horizontal Axis Pelton Turbines

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis Numerical and Experimental Investigation of Flow in Horizontal Axis Pelton Turbines by : Sean Petley

Download or read book Numerical and Experimental Investigation of Flow in Horizontal Axis Pelton Turbines written by Sean Petley and published by . This book was released on 2019 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of Heat Transfer in Separated Flow on a Highly Loaded LP Turbine Cascade

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ISBN 13 :
Total Pages : 11 pages
Book Rating : 4.:/5 (742 download)

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Book Synopsis Experimental Investigation of Heat Transfer in Separated Flow on a Highly Loaded LP Turbine Cascade by :

Download or read book Experimental Investigation of Heat Transfer in Separated Flow on a Highly Loaded LP Turbine Cascade written by and published by . This book was released on 2003 with total page 11 pages. Available in PDF, EPUB and Kindle. Book excerpt: Today aerodynamic design tools and CFD-codes provide excellent quality in predicting 2D and 3D flows in turbine components. Nevertheless correlation and numerical methods are not able to predict beat flux in a satisfactory accuracy for complex heat transfer problems for example 3D film cooling mixing zones or areas of separated flow. In order to close part of these gaps in knowledge and to improve the understanding of the interaction between the flow pattern and the beat transfer phenomena experimental investigations were carried out focused on 2D separated flow on the pressure side leading edge of the highly loaded low pressure turbine cascade named T106-300. The cascade was instrumented with pressure taps and glue-on hot-film sensors. The pressure taps provided the static profile pressure distribution. The hot-film anemometry technique normally is used to detect boundary layer development; moreover a procedure will be presented to evaluate the heat transfer coefficient as well. Supplementary boundary layer traverses with a 1D hot-wire probe were carried out at positions inside and downstream of the separation. The dimension of the separation tip to 60% chord was varied by the incidence angle. By variation of Reynolds number and Mach number a data set is available which will be put down to a correlation.

Applied mechanics reviews

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ISBN 13 :
Total Pages : 400 pages
Book Rating : 4.3/5 (243 download)

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Book Synopsis Applied mechanics reviews by :

Download or read book Applied mechanics reviews written by and published by . This book was released on 1948 with total page 400 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA SP.

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ISBN 13 :
Total Pages : 590 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA SP. by :

Download or read book NASA SP. written by and published by . This book was released on 1993 with total page 590 pages. Available in PDF, EPUB and Kindle. Book excerpt: