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Effect Of Stage Spacing On Performance Of 375 Inch Mean Diameter Two Stage Turbine Having Partial Admission In The First Stage
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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
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].
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:
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.
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:
Book Synopsis Analytical Investigation of Performance of Two-stage Turbine Over a Range of Ratios of Specific Heats from 1.2 to 1 2/3 by : Warren J. Whitney
Download or read book Analytical Investigation of Performance of Two-stage Turbine Over a Range of Ratios of Specific Heats from 1.2 to 1 2/3 written by Warren J. Whitney and published by . This book was released on 1962 with total page 50 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
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:
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:
Book Synopsis Design and Performance of a Six-stage 8-inch-mean-diameter Reentry Turbine by :
Download or read book Design and Performance of a Six-stage 8-inch-mean-diameter Reentry Turbine written by and published by . This book was released on 1962 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Air-performance Evaluation of a 4.0-inch-mean-diameter Single-stage Turbine at Various Inlet Pressures from 0.14 to 1.88 Atmospheres and Corresponding Reynolds Numbers from 2500 to 50,000 by : Robert Y. Wong
Download or read book Air-performance Evaluation of a 4.0-inch-mean-diameter Single-stage Turbine at Various Inlet Pressures from 0.14 to 1.88 Atmospheres and Corresponding Reynolds Numbers from 2500 to 50,000 written by Robert Y. Wong and published by . This book was released on 1962 with total page 39 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Experimental Investigation of a 3.0-inch-mean-diameter Full-admission Three-stage Turbine Suitable for Small Auxiliary Power Units by : Robert Y. 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 Y. Wong and published by . This book was released on 1965 with total page 21 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Book Synopsis Effects of Partial Admission on Performance of a Gas Turbine by : Robert C. Kohl
Download or read book Effects of Partial Admission on Performance of a Gas Turbine written by Robert C. Kohl and published by . This book was released on 1949 with total page 76 pages. Available in PDF, EPUB and Kindle. Book excerpt: In successive studies, a representative single-stage full-admission gas turbine was operated with full and 120 dgree peripheral admission, and the turbine performances at these operating conditions are compared.
Book Synopsis Analytical Investigation of Performance of Two-stage Turbine Over a Range of Ratios of Specific Heats from 1.2 to 1 2/3 by : Warren J. Whitney
Download or read book Analytical Investigation of Performance of Two-stage Turbine Over a Range of Ratios of Specific Heats from 1.2 to 1 2/3 written by Warren J. Whitney and published by . This book was released on 1962 with total page 46 pages. Available in PDF, EPUB and Kindle. Book excerpt:
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:
Book Synopsis Analytical Investigation of the Effect of Cooling Air on Two-stage Turbine Performance by : Warren J. Whitney
Download or read book Analytical Investigation of the Effect of Cooling Air on Two-stage Turbine Performance written by Warren J. Whitney and published by . This book was released on 1969 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt:
