Removal of Secondary-flow Accumulations in a Two-dimensional Turbine Nozzle Passage by Boundary-layer Bleed

Removal of Secondary-flow Accumulations in a Two-dimensional Turbine Nozzle Passage by Boundary-layer Bleed
Author :
Publisher :
Total Pages : 20
Release :
ISBN-10 : OCLC:1109540342
ISBN-13 :
Rating : 4/5 (42 Downloads)

Book Synopsis Removal of Secondary-flow Accumulations in a Two-dimensional Turbine Nozzle Passage by Boundary-layer Bleed by : Robert Y. Wong

Download or read book Removal of Secondary-flow Accumulations in a Two-dimensional Turbine Nozzle Passage by Boundary-layer Bleed written by Robert Y. Wong and published by . This book was released on 1955 with total page 20 pages. Available in PDF, EPUB and Kindle. Book excerpt:


Removal of Secondary-flow Accumulations in a Two-dimensional Turbine Nozzle Passage by Boundary-layer Bleed Related Books

Removal of Secondary-flow Accumulations in a Two-dimensional Turbine Nozzle Passage by Boundary-layer Bleed
Language: en
Pages: 20
Comparison of Secondary Flows and Boundary-layer Accumulations in Several Turbine Nozzles
Language: en
Pages: 68
Authors: Milton G. Kofskey
Categories: Air flow
Type: BOOK - Published: 1953 - Publisher:

DOWNLOAD EBOOK

An investigation of secondary-flow loss cores originating in turbine nozzle blade passages was conducted by means of flow visualization studies and detailed flo
NACA Research Memorandum
Language: en
Pages: 618
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1955 - Publisher:

DOWNLOAD EBOOK

Research Abstracts and Reclassification Notice
Language: en
Pages: 716
Authors: United States. National Advisory Committee for Aeronautics
Categories: Aeronautics
Type: BOOK - Published: 1956 - Publisher:

DOWNLOAD EBOOK

Study of Secondary-flow Patterns in an Annular Cascade of Turbine Nozzle Blades with Vortex Design
Language: en
Pages: 38
Authors: Harold E. Rohlik
Categories: Air flow
Type: BOOK - Published: 1953 - Publisher:

DOWNLOAD EBOOK

In order to increase understanding of the origin of losses in a turbine, the secondary-flow components in the boundary layers and the blade wakes of an annular