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Autorotation of thin plates Andersen, Fabian
Abstract
A visualization technique is applied to the unsteady separated flow about an autorotatlng flat plate. An unsteady potential model is attempted to predict the pressure loading on the plate as a function of angle of attack. To visualize the flow, a streakline is marked by low density air created by the wake of a heated wire probe. An off-center parabolic mirror Schlieren system detects the density gradient. Due to the highly unsteady nature (in this project, the plate rotates at almost 1,000 r.p.m. for a 10-foot per second freestream velocity) of the flow, high-speed 35mm, single lens reflex shots or 16mm. movie films recorded the image. Timing marks on the movie film provided information of the angular speed of the plate during acceleration to the autorotation speed and at autorotation. The two-dimensional unsteady attached flow model attempts to duplicate the effects of separation by superimposing vortices in the wake, as shown in the flow visualization, and by eliminating terms representing the freestream velocity in the range of 60 to 150 degrees angle of attack.
Item Metadata
Title |
Autorotation of thin plates
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Creator | |
Publisher |
University of British Columbia
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Date Issued |
1970
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Description |
A visualization technique is applied to the unsteady separated flow about an autorotatlng flat plate. An unsteady potential model is attempted to predict the pressure loading on the plate as a function of angle of attack.
To visualize the flow, a streakline is marked by low density air created by the wake of a heated wire probe. An off-center parabolic mirror Schlieren system detects the density gradient. Due to the highly unsteady nature (in this project, the plate rotates at almost 1,000 r.p.m. for a 10-foot per second freestream velocity) of the flow, high-speed 35mm, single lens reflex shots or 16mm. movie films recorded the image.
Timing marks on the movie film provided information of the angular speed of the plate during acceleration to the autorotation speed and at autorotation.
The two-dimensional unsteady attached flow model attempts to duplicate the effects of separation by superimposing vortices in the wake, as shown in the flow visualization, and by eliminating terms representing the freestream velocity in the range of 60 to 150 degrees angle of attack.
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Genre | |
Type | |
Language |
eng
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Date Available |
2011-05-25
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Provider |
Vancouver : University of British Columbia Library
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Rights |
For non-commercial purposes only, such as research, private study and education. Additional conditions apply, see Terms of Use https://open.library.ubc.ca/terms_of_use.
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DOI |
10.14288/1.0102204
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URI | |
Degree | |
Program | |
Affiliation | |
Degree Grantor |
University of British Columbia
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Campus | |
Scholarly Level |
Graduate
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Aggregated Source Repository |
DSpace
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Item Media
Item Citations and Data
Rights
For non-commercial purposes only, such as research, private study and education. Additional conditions apply, see Terms of Use https://open.library.ubc.ca/terms_of_use.