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Cavitation and wake structure of uns...
~
Hart, Douglas Payton.
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Cavitation and wake structure of unsteady tip vortex flows.
Record Type:
Language materials, printed : Monograph/item
Title/Author:
Cavitation and wake structure of unsteady tip vortex flows./
Author:
Hart, Douglas Payton.
Description:
250 p.
Notes:
Co-Advisers: Allan Acosta; Christopher Brennen.
Contained By:
Dissertation Abstracts International55-05B.
Subject:
Engineering, Aerospace. -
Online resource:
http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=9427296
Cavitation and wake structure of unsteady tip vortex flows.
Hart, Douglas Payton.
Cavitation and wake structure of unsteady tip vortex flows.
- 250 p.
Co-Advisers: Allan Acosta; Christopher Brennen.
Thesis (Ph.D.)--California Institute of Technology, 1993.
Unsteady flows are prevalent in virtually every fluid application yet, because of their intrinsic complexity, few attempts have been made to measure them or explain their behavior. This thesis presents an experimental study of one of the simplest unsteady flow induced effects, the periodic change in angle of attack of a lifting surface. Of particular interest is the influence this effect has on the tip vortex structure of a finite aspect ratio hydrofoil and the part it plays in the inception of cavitation.Subjects--Topical Terms:
1018395
Engineering, Aerospace.
Cavitation and wake structure of unsteady tip vortex flows.
LDR
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Hart, Douglas Payton.
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Cavitation and wake structure of unsteady tip vortex flows.
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250 p.
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Co-Advisers: Allan Acosta; Christopher Brennen.
500
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Source: Dissertation Abstracts International, Volume: 55-05, Section: B, page: 1968.
502
$a
Thesis (Ph.D.)--California Institute of Technology, 1993.
520
$a
Unsteady flows are prevalent in virtually every fluid application yet, because of their intrinsic complexity, few attempts have been made to measure them or explain their behavior. This thesis presents an experimental study of one of the simplest unsteady flow induced effects, the periodic change in angle of attack of a lifting surface. Of particular interest is the influence this effect has on the tip vortex structure of a finite aspect ratio hydrofoil and the part it plays in the inception of cavitation.
520
$a
An aspect ratio 2.3 hydrofoil was reflection-plane mounted to the test section floor of the Caltech Low Turbulence Water Tunnel and harmonically oscillated in pitch near its center of pressure. Observations of the growth and collapse of surface and tip vortex cavitation were made along with detailed observations of the interaction of the tip vortex formation with the spanwise wake structure. Measurements of the cavitation inception number for surface cavitation and tip vortex cavitation were made relative to the phase of the hydrofoil and the reduced frequency, k = $\omega
$c
/2U$\sb{\infty}$, of oscillation. Studies of the oscillation-induced spanwise trailing vortex structures and the Karman vortex street generated by the boundary layer were made of a two-dimensional hydrofoil. Laser Doppler Velocimetry (LDV) measurements were taken of the tip vortex velocity profile and the flow at the trailing edge of both the two- and the three-dimensional hydrofoils at reduced frequencies ranging from 0.5 to 2.0. Dynamic changes in bound circulation and shed vorticity in the streamwise and spanwise directions relative to the freestream were calculated from these measurements at three locations along the span of the foil. The results of these measurements are compared to theoretical flow calculations and related to measurements of the cavitation inception number in the tip vortex region of the three-dimensional foil.
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School code: 0037.
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Engineering, Aerospace.
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1018395
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Engineering, Marine and Ocean.
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Physics, Fluid and Plasma.
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California Institute of Technology.
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55-05B.
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0037
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Acosta, Allan,
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advisor
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Brennen, Christopher,
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advisor
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Ph.D.
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1993
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http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=9427296
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