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naca-tn-2834

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National Advisory Committee for Aeronautics, Technical Notes - Flow Surfaces in Rotating Axial Flow Passages

In order to investigate the deviation of flow surfaces from their
assumed orientation in the usual type of two-dimensional solution, three-
dimensional, incompressible, nonviscous, absolute irrotational fluid
motion is determined for flow through rotating axial—flow passages
bounded by straight blades of finite spacing and infinite axial length
lying on meridional planes. Solutions are obtained for five passages
with varying blade spacing and hub-tip ratio. The results are presented
in such a manner as to apply for all ratios of axial velocity to passage
tip speed. It is concluded that, for conditions in typical axial-flow
blade rows, the deviation of flow surfaces from their assumed orienta-
tion in two-dimensional solutions is small.

A flow surface in the passage between two blades of a compressor
or turbine is generated by the motion through the passage of any fluid
line consisting of the same fluid particles and extending from one
boundary to another in a plane normal to the axis of rotation. In two-
dimensional analyses of flow in compressors and turbines, the fluid
motion is usually assumed to occur on flow surfaces that are: (1) sur-
faces of revolution about the axis of the turbomachine (blade—to4blade
solutions, references 1 and 2, for example) or (2) mean passage surfaces
that are congruent with the mean blade surfaces (hub—to—shroud solutions,
references 5 and 4, for example). Actually, the flow surfaces deviate
from the orientation assumed for the two-dimensional solutions and, in
the direction of flow, become progressively more tilted and distorted.

This deviation of the flow surfaces from.their assumed orientation is
caused by spanwise variations of blade loading and, in rotating blade
rows, by rotation of the fluid particles relative to the passage in a
plane normal to the axis of the'blade row. This rotation is required
to maintain the rotational or irrotational character of the absolute
fluid motion.

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naca-tn-2834

  • Version
  • 94 Downloads
  • 1,004.78 KB File Size
  • 1 File Count
  • January 17, 2017 Create Date
  • January 17, 2017 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Technical Notes - Flow Surfaces in Rotating Axial Flow Passages

In order to investigate the deviation of flow surfaces from their
assumed orientation in the usual type of two-dimensional solution, three-
dimensional, incompressible, nonviscous, absolute irrotational fluid
motion is determined for flow through rotating axial—flow passages
bounded by straight blades of finite spacing and infinite axial length
lying on meridional planes. Solutions are obtained for five passages
with varying blade spacing and hub-tip ratio. The results are presented
in such a manner as to apply for all ratios of axial velocity to passage
tip speed. It is concluded that, for conditions in typical axial-flow
blade rows, the deviation of flow surfaces from their assumed orienta-
tion in two-dimensional solutions is small.

A flow surface in the passage between two blades of a compressor
or turbine is generated by the motion through the passage of any fluid
line consisting of the same fluid particles and extending from one
boundary to another in a plane normal to the axis of rotation. In two-
dimensional analyses of flow in compressors and turbines, the fluid
motion is usually assumed to occur on flow surfaces that are: (1) sur-
faces of revolution about the axis of the turbomachine (blade—to4blade
solutions, references 1 and 2, for example) or (2) mean passage surfaces
that are congruent with the mean blade surfaces (hub—to—shroud solutions,
references 5 and 4, for example). Actually, the flow surfaces deviate
from the orientation assumed for the two-dimensional solutions and, in
the direction of flow, become progressively more tilted and distorted.

This deviation of the flow surfaces from.their assumed orientation is
caused by spanwise variations of blade loading and, in rotating blade
rows, by rotation of the fluid particles relative to the passage in a
plane normal to the axis of the'blade row. This rotation is required
to maintain the rotational or irrotational character of the absolute
fluid motion.

FileAction
naca-tn-2834 Flow Surfaces in Rotating Axial Flow Passages.pdfDownload 
17,005 Documents in our Technical Library
2728513 Total Downloads

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Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...

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