Design and Experimental Performance of a Two Stage Partial Admission Turbine

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ISBN 13 :
Total Pages : 168 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Design and Experimental Performance of a Two Stage Partial Admission Turbine by :

Download or read book Design and Experimental Performance of a Two Stage Partial Admission Turbine written by and published by . This book was released on 1992 with total page 168 pages. Available in PDF, EPUB and Kindle. Book excerpt: A three-inch mean diameter, two-stage turbine with partial admission in each stage was experimentally investigated over a range of admissions and angular orientations of admission arcs. Three configurations were tested in which first stage admission varied from 37.4 percent (10 of 29 passages open, 5 per side) to 6.9 percent (2 open, 1 per side). Corresponding second stage admissions were 45.2 percent (14 of 31 passages open, 7 per side) and 12.9 percent (4 open, 2 per side). Angular positions of the second state admission arcs with respect to the first stage varied over a range of 70 degrees. Design and off-design efficiency and flow characteristics for the three configurations are presented. The results indicated that peak efficiency and the corresponding isentropic velocity ratio decreased as the arcs of admission were decreased. Both efficiency and flow characteristics were sensitive to the second stage nozzle orientation angles. Turbine performance, Two-stage partial admission turbine, Impulse turbine.

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:

Experimental Investigation of the Partial- Admission Performance Characteristics of a Single-stage Mach 2 Supersonic Turbine

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ISBN 13 :
Total Pages : 20 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Experimental Investigation of the Partial- Admission Performance Characteristics of a Single-stage Mach 2 Supersonic Turbine by : Thomas P. Moffitt

Download or read book Experimental Investigation of the Partial- Admission Performance Characteristics of a Single-stage Mach 2 Supersonic Turbine written by Thomas P. Moffitt and published by . This book was released on 1959 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Design of Turbine and Experimental Performance of First Two Stages

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ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Design of Turbine and Experimental Performance of First Two Stages by : Harold E. Rohlik

Download or read book Design of Turbine and Experimental Performance of First Two Stages written by Harold E. Rohlik and published by . This book was released on 1961 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect of Stage Spacing on Performance of 3.75-inch-mean-diameter Two-stage Turbine Having Partial Admission in the First Stage

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ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Effect of Stage Spacing on Performance of 3.75-inch-mean-diameter Two-stage Turbine Having Partial Admission in the First Stage by : William J. Nusbaum

Download or read book Effect of Stage Spacing on Performance of 3.75-inch-mean-diameter Two-stage Turbine Having Partial Admission in the First Stage written by William J. Nusbaum and published by . This book was released on 1964 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt: "The design and the experimental investigation of a 3.75-inch-mean-diameter partial-admission two-stage turbine are presented herein. The investigation was made to determine the effect on two-stage-turbine performance of a change in the axial distance between stages for a turbine with partial admission in the first stage. Accordingly, the turbine was designed with 31.3-percent admission in the first stage, full admission in the second stage, and provision for changing the axial distance between stages. The results of the two-stage investigation are presented for each of the axial distances between stages of 0.25, 0.50, 0.75, 1.00, 1.50, and 2.00 inches. The results of the first-stage investigation are also presented, together with a calculated efficiency for the second stage, at each value of stage spacing as calculated from the two-stage and first-stage results."--Page 1

Experimental Investigation of Partial and Full-admission Characteristics of a Two- Stage Velocity-compound Turbine

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ISBN 13 :
Total Pages : 28 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Experimental Investigation of Partial and Full-admission Characteristics of a Two- Stage Velocity-compound Turbine by :

Download or read book Experimental Investigation of Partial and Full-admission Characteristics of a Two- Stage Velocity-compound Turbine written by and published by . This book was released on 1960 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of a 3.0-inch-mean-diameter Full-admission Three-stage Turbine Suitable for Small Auxiliary Power Units

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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 a 3.0-inch-mean-diameter Full-admission Three-stage Turbine Suitable for Small Auxiliary Power Units by : Robert Young Wong

Download or read book Experimental Investigation of a 3.0-inch-mean-diameter Full-admission Three-stage Turbine Suitable for Small Auxiliary Power Units written by Robert Young Wong and published by . This book was released on 1965 with total page 26 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of the Partial- Admission Performance Characteristics of a Single-stage Mach 2 Supersonic Turbine

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ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Experimental Investigation of the Partial- Admission Performance Characteristics of a Single-stage Mach 2 Supersonic Turbine by :

Download or read book Experimental Investigation of the Partial- Admission Performance Characteristics of a Single-stage Mach 2 Supersonic Turbine written by and published by . This book was released on 1959 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Design of Turbine and Experimental Performance of First Two Stages

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ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.:/5 (761 download)

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Book Synopsis Design of Turbine and Experimental Performance of First Two Stages by : Harold E. Rohlik

Download or read book Design of Turbine and Experimental Performance of First Two Stages written by Harold E. Rohlik and published by . This book was released on 1961 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Effect of Stage Spacing on Performance of 3.75-inch-mean-diameter Two-stage Turbine Having Partial Admission in the First Stage

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ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (76 download)

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Book Synopsis Effect of Stage Spacing on Performance of 3.75-inch-mean-diameter Two-stage Turbine Having Partial Admission in the First Stage by : William J. Nusbaum

Download or read book Effect of Stage Spacing on Performance of 3.75-inch-mean-diameter Two-stage Turbine Having Partial Admission in the First Stage written by William J. Nusbaum and published by . This book was released on 1964 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: "The design and the experimental investigation of a 3.75-inch-mean-diameter partial-admission two-stage turbine are presented herein. The investigation was made to determine the effect on two-stage-turbine performance of a change in the axial distance between stages for a turbine with partial admission in the first stage. Accordingly, the turbine was designed with 31.3-percent admission in the first stage, full admission in the second stage, and provision for changing the axial distance between stages. The results of the two-stage investigation are presented for each of the axial distances between stages of 0.25, 0.50, 0.75, 1.00, 1.50, and 2.00 inches. The results of the first-stage investigation are also presented, together with a calculated efficiency for the second stage, at each value of stage spacing as calculated from the two-stage and first-stage results."--Page [1].

Performance Evaluation of a Two-stage Turbine Designed for a Ratio of Blade Speed to Jet Speed of 0.146

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ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Performance Evaluation of a Two-stage Turbine Designed for a Ratio of Blade Speed to Jet Speed of 0.146 by : Milton G. Kofskey

Download or read book Performance Evaluation of a Two-stage Turbine Designed for a Ratio of Blade Speed to Jet Speed of 0.146 written by Milton G. Kofskey and published by . This book was released on 1960 with total page 42 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 : 22 pages
Book Rating : 4.:/5 (76 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 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Performance Evaluation of a Two-stage Turbine Designed for a Ratio of Blade Speed to Jet Speed of 0.146

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ISBN 13 :
Total Pages : 42 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Performance Evaluation of a Two-stage Turbine Designed for a Ratio of Blade Speed to Jet Speed of 0.146 by :

Download or read book Performance Evaluation of a Two-stage Turbine Designed for a Ratio of Blade Speed to Jet Speed of 0.146 written by and published by . This book was released on 1960 with total page 42 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Design and Experimental Investigation of Two Rotor Blade Modifications for a High-weight-flow Low-pressure-ratio Turbine

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ISBN 13 :
Total Pages : 32 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Design and Experimental Investigation of Two Rotor Blade Modifications for a High-weight-flow Low-pressure-ratio Turbine by : Robert R. Nunamaker

Download or read book Design and Experimental Investigation of Two Rotor Blade Modifications for a High-weight-flow Low-pressure-ratio Turbine written by Robert R. Nunamaker and published by . This book was released on 1959 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Technical Note

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ISBN 13 :
Total Pages : 314 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Technical Note by :

Download or read book NASA Technical Note written by and published by . This book was released on 1965 with total page 314 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Scientific and Technical Aerospace Reports

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ISBN 13 :
Total Pages : 1028 pages
Book Rating : 4.3/5 (91 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 1994 with total page 1028 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Design and Experimental Investigation of a Single-stage Turbine with a Rotor Entering Relative Mach Number of 2

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ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Design and Experimental Investigation of a Single-stage Turbine with a Rotor Entering Relative Mach Number of 2 by : Thomas P. Moffitt

Download or read book Design and Experimental Investigation of a Single-stage Turbine with a Rotor Entering Relative Mach Number of 2 written by Thomas P. Moffitt and published by . This book was released on 1958 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt: