Singular partial integro-differential equations arising in thin aerofoil theory
Singular partial integro-differential equations arising in thin aerofoil theory
A study is undertaken of three physical problems in which singular partial integro-differential equations arise. The equations result from applying thin aerofoil theory to two-dimensional potential flow over a free boundary. In all cases the work builds on existing steady models, for which ordinary singular integro-differential equations have been derived, to obtain time-dependent equations. The first of the physical problems examined is the sail equation, which describes the behaviour of a thin, flexible, inextensible sail in a high-Reynolds-number cross-flow at a small, but time-dependent, angle of incidence to the sail. A review of literature on the sail problem is presented. The unsteady equation is then solved numerically for various angles of incidence and sail masses. Variations of the unsteady sail equation are also derived to describe the sail as the sail mass becomes very small or very large, and to describe the flapping of a flag. An analytic expression is found for the low-mass sail given a particular set of functions for the angle of attack, for which the tension in the sail, and hence the lift, are zero.
The second problem examined is that of slot injection into a high-Reynolds-number cross-flow driven by an excess pressure in the slot. A literature review of slot injection to, and suction from, a free stream is presented, and then the unsteady injection problem is considered. Three different regimes are found for slot injection, according to the time scale of the pressure variations. Of these, the most important is the 'interactive' time scale, for which a third order singular partial integro-differential equation is obtained for the height of the shear layer separating the injected fluid from the free stream. For the other two cases, analytic solutions are found in terms of the known steady solutions.
University of Southampton
Lattimer, Timothy Richard Bislig
b2d24b77-ed5b-412a-8d29-619864244109
1996
Lattimer, Timothy Richard Bislig
b2d24b77-ed5b-412a-8d29-619864244109
Lattimer, Timothy Richard Bislig
(1996)
Singular partial integro-differential equations arising in thin aerofoil theory.
University of Southampton, Doctoral Thesis.
Record type:
Thesis
(Doctoral)
Abstract
A study is undertaken of three physical problems in which singular partial integro-differential equations arise. The equations result from applying thin aerofoil theory to two-dimensional potential flow over a free boundary. In all cases the work builds on existing steady models, for which ordinary singular integro-differential equations have been derived, to obtain time-dependent equations. The first of the physical problems examined is the sail equation, which describes the behaviour of a thin, flexible, inextensible sail in a high-Reynolds-number cross-flow at a small, but time-dependent, angle of incidence to the sail. A review of literature on the sail problem is presented. The unsteady equation is then solved numerically for various angles of incidence and sail masses. Variations of the unsteady sail equation are also derived to describe the sail as the sail mass becomes very small or very large, and to describe the flapping of a flag. An analytic expression is found for the low-mass sail given a particular set of functions for the angle of attack, for which the tension in the sail, and hence the lift, are zero.
The second problem examined is that of slot injection into a high-Reynolds-number cross-flow driven by an excess pressure in the slot. A literature review of slot injection to, and suction from, a free stream is presented, and then the unsteady injection problem is considered. Three different regimes are found for slot injection, according to the time scale of the pressure variations. Of these, the most important is the 'interactive' time scale, for which a third order singular partial integro-differential equation is obtained for the height of the shear layer separating the injected fluid from the free stream. For the other two cases, analytic solutions are found in terms of the known steady solutions.
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Published date: 1996
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Local EPrints ID: 462962
URI: http://eprints.soton.ac.uk/id/eprint/462962
PURE UUID: ab2c07f6-55fb-4f73-86a3-19ec30237607
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Date deposited: 04 Jul 2022 20:31
Last modified: 16 Mar 2024 19:00
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Author:
Timothy Richard Bislig Lattimer
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