Comparison of secondary flows and boundary-layer accumulations in several turbine nozzles / Milton G. Kofskey, Hubert W. Allen, and Howard Z. Herzig.
An investigation of secondary-flow loss cores originating in turbine nozzle blade passages was conducted by means of flow visualization studies and detailed flow measurements. The degree of which blade surface velocity profiles affect the magnitude and concentration of loss cores was investigated by...
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Other title: | Technical report archive and image library. |
Format: | Government Document Book |
Language: | English |
Published: |
Washington, D.C. :
National Advisory Committee for Aeronautics,
1953.
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Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
2989. |
Subjects: |
MARC
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100 | 1 | |a Kofskey, Milton G. |0 http://id.loc.gov/authorities/names/no2008161471 |1 http://isni.org/isni/0000000050542124. | |
245 | 1 | 0 | |a Comparison of secondary flows and boundary-layer accumulations in several turbine nozzles / |c Milton G. Kofskey, Hubert W. Allen, and Howard Z. Herzig. |
260 | |a Washington, D.C. : |b National Advisory Committee for Aeronautics, |c 1953. | ||
300 | |a 58 pages : |b illustrations, tables ; |c 28 cm. | ||
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490 | 1 | |a National Advisory Committee for Aeronautics ; |v no. 2989. | |
500 | |a "August 1953." | ||
500 | |a NACA TN Number 2989. | ||
504 | |a Includes bibliographical references. | ||
520 | 3 | |a An investigation of secondary-flow loss cores originating in turbine nozzle blade passages was conducted by means of flow visualization studies and detailed flow measurements. The degree of which blade surface velocity profiles affect the magnitude and concentration of loss cores was investigated by comparing three nozzle blade configurations. | |
583 | 1 | |a will digitize |c 20121201 |z Queued for digitization December 1, 2012 |2 pda |5 miu. | |
650 | 0 | |a Turbines |x Blades. |0 http://id.loc.gov/authorities/subjects/sh85138720. | |
650 | 0 | |a Turbomachines |x Blades. |0 http://id.loc.gov/authorities/subjects/sh85138744. | |
650 | 0 | |a Nozzles. |0 http://id.loc.gov/authorities/subjects/sh85092916. | |
650 | 0 | |a Air flow. |0 http://id.loc.gov/authorities/subjects/sh85002635. | |
650 | 0 | |a Flow visualization. |0 http://id.loc.gov/authorities/subjects/sh85049293. | |
650 | 0 | |a Boundary layer. |0 http://id.loc.gov/authorities/subjects/sh85016095. | |
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650 | 7 | |a Nozzles. |2 fast |0 (OCoLC)fst01039825. | |
650 | 7 | |a Turbines |x Blades. |2 fast |0 (OCoLC)fst01159117. | |
650 | 7 | |a Turbomachines |x Blades. |2 fast |0 (OCoLC)fst01159179. | |
700 | 1 | |a Allen, Hubert W. | |
700 | 1 | |a Herzig, Howard Z. | |
710 | 1 | |a United States. |b National Advisory Committee for Aeronautics. |0 http://id.loc.gov/authorities/names/n79060141 |1 http://isni.org/isni/0000000106642010. | |
730 | 0 | |a Technical report archive and image library. |0 http://id.loc.gov/authorities/names/no2008179973. | |
776 | 0 | 8 | |i Online version: |a Kofskey, Milton G. |t Comparison of secondary flows and boundary-layer accumulations in several turbine nozzles. |d Washington, D.C. : National Advisory Committee for Aeronautics, 1953 |w (OCoLC)885132448. |
830 | 0 | |a Technical note (United States. National Advisory Committee for Aeronautics) ; |v 2989. |0 http://id.loc.gov/authorities/names/no2009017392. | |
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