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

Effect of Stage Spacing on Performance of 3.75-inch-mean-diameter Two-stage Turbine Having Partial Admission in the First Stage
Author: William J. Nusbaum
Publisher:
Total Pages: 32
Release: 1964
Genre: Gas-turbines
ISBN:

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"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


Effect of Stage Spacing on Performance of 3.75-inch-mean-diameter Two-stage Turbine Having Partial Admission in the First Stage
Language: en
Pages: 32
Authors: William J. Nusbaum
Categories: Gas-turbines
Type: BOOK - Published: 1964 - Publisher:

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"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
Effect of Stage Spacing on Performance of 3.75-inch-mean-diameter Two-stage Turbine Having Partial Admission in the First Stage
Language: en
Pages: 22
Authors: William J. Nusbaum
Categories: Gas-turbines
Type: BOOK - Published: 1964 - Publisher:

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"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
Experimental Investigation of Partial- and Full-admission Characteristics of a Two-stage Velocity-compounded Turbine
Language: en
Pages: 26
Authors: Thomas P. Moffitt
Categories: Turbines
Type: BOOK - Published: 1960 - Publisher:

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Design and Experimental Performance of a Two Stage Partial Admission Turbine
Language: en
Pages: 168
Authors:
Categories:
Type: BOOK - Published: 1992 - Publisher:

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A three-inch mean diameter, two-stage turbine with partial admission in each stage was experimentally investigated over a range of admissions and angular orient
Performance Evaluation of a Two-stage Turbine Designed for a Ratio of Blade Speed to Jet Speed of 0.146
Language: en
Pages: 42
Authors: Milton G. Kofskey
Categories: Liquid propellant rocket engines
Type: BOOK - Published: 1960 - Publisher:

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