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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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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Author : William J. Nusbaum
language : en
Publisher:
Release Date : 1964
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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Gas-turbines categories.
"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
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Author : William J. Nusbaum
language : en
Publisher:
Release Date : 1964
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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Gas-turbines categories.
"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].
Design Of Turbine And Experimental Performance Of First Two Stages
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Author : Harold E. Rohlik
language : en
Publisher:
Release Date : 1961
Design Of Turbine And Experimental Performance Of First Two Stages written by Harold E. Rohlik and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1961 with Stages (Rocketry) categories.
Analytical Investigation Of Performance Of Two Stage Turbine Over A Range Of Ratios Of Specific Heats From 1 2 To 1 2 3
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Author : Warren J. Whitney
language : en
Publisher:
Release Date : 1962
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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1962 with Turbines categories.
Experimental Investigation Of Partial And Full Admission Characteristics Of A Two Stage Velocity Compounded Turbine
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Author : Thomas P. Moffitt
language : en
Publisher:
Release Date : 1960
Experimental Investigation Of Partial And Full Admission Characteristics Of A Two Stage Velocity Compounded Turbine written by Thomas P. Moffitt and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Turbines categories.
Performance Evaluation Of A Two Stage Turbine Designed For A Ratio Of Blade Speed To Jet Speed Of 0 146
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Author : Milton G. Kofskey
language : en
Publisher:
Release Date : 1960
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 has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with Liquid propellant rocket engines categories.
Design And Experimental Performance Of A Two Stage Partial Admission Turbine
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Author :
language : en
Publisher:
Release Date : 1992
Design And Experimental Performance Of A Two Stage Partial Admission Turbine written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1992 with categories.
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 Compound Turbine
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Author :
language : en
Publisher:
Release Date : 1960
Experimental Investigation Of Partial And Full Admission Characteristics Of A Two Stage Velocity Compound Turbine written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1960 with categories.
Experimental Investigation Of The Partial Admission Performance Characteristics Of A Single Stage Mach 2 Supersonic Turbine
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Author :
language : en
Publisher:
Release Date : 1959
Experimental Investigation Of The Partial Admission Performance Characteristics Of A Single Stage Mach 2 Supersonic Turbine written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1959 with categories.
Nasa Technical Note
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Author :
language : en
Publisher:
Release Date : 1964
Nasa Technical Note written by and has been published by this book supported file pdf, txt, epub, kindle and other format this book has been release on 1964 with Aeronautics categories.