<?xml version="1.0" encoding="UTF-8"?><?xml-stylesheet type="text/xsl" href="static/style.xsl"?><OAI-PMH xmlns="http://www.openarchives.org/OAI/2.0/" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xsi:schemaLocation="http://www.openarchives.org/OAI/2.0/ http://www.openarchives.org/OAI/2.0/OAI-PMH.xsd"><responseDate>2026-09-19T04:29:04Z</responseDate><request verb="GetRecord" identifier="oai:dspace.mit.edu:1721.1/38699" metadataPrefix="dim">https://dspace.mit.edu/server/oai/request</request><GetRecord><record><header><identifier>oai:dspace.mit.edu:1721.1/38699</identifier><datestamp>2022-01-13T07:54:36Z</datestamp><setSpec>com_1721.1_7582</setSpec><setSpec>com_1721.1_7581</setSpec><setSpec>col_1721.1_131022</setSpec></header><metadata><dim:dim xmlns:dim="http://www.dspace.org/xmlns/dspace/dim" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance" xmlns:doc="http://www.lyncode.com/xoai" xsi:schemaLocation="http://www.dspace.org/xmlns/dspace/dim http://www.dspace.org/schema/dim.xsd">
   <dim:field mdschema="dc" element="contributor" qualifier="advisor" lang="en_US">Jerome J. Milgram.</dim:field>
   <dim:field mdschema="dc" element="contributor" qualifier="author" lang="en_US">Cairoli, Claudio, 1975-</dim:field>
   <dim:field mdschema="dc" element="contributor" qualifier="other" lang="en_US">Massachusetts Institute of Technology. Dept. of Mechanical Engineering.</dim:field>
   <dim:field mdschema="dc" element="contributor" qualifier="department">Massachusetts Institute of Technology. Department of Mechanical Engineering</dim:field>
   <dim:field mdschema="dc" element="date" qualifier="accessioned">2007-08-29T20:46:35Z</dim:field>
   <dim:field mdschema="dc" element="date" qualifier="available">2007-08-29T20:46:35Z</dim:field>
   <dim:field mdschema="dc" element="date" qualifier="copyright" lang="en_US">2007</dim:field>
   <dim:field mdschema="dc" element="date" qualifier="issued" lang="en_US">2007</dim:field>
   <dim:field mdschema="dc" element="identifier" qualifier="uri">http://hdl.handle.net/1721.1/38699</dim:field>
   <dim:field mdschema="dc" element="identifier" qualifier="oclc" lang="en_US">165169203</dim:field>
   <dim:field mdschema="dc" element="description" lang="en_US">Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 2007.</dim:field>
   <dim:field mdschema="dc" element="description" lang="en_US">Includes bibliographical references (leaves 111-114).</dim:field>
   <dim:field mdschema="dc" element="description" qualifier="abstract" lang="en_US">In this thesis, a theoretical and numerical procedure for predicting the effects of viscosity on the hydrodynamic forces developed by a sailing yacht hull is presented. A simultaneous viscous/inviscid algorithm is developed by coupling a low order panel method with quasi three-dimensional integral boundary layer equations. A transom condition is used to prevent non-zero wave heights at the stern for a hull with overhangs. The influence of viscosity on the outer inviscid flow is modeled using a wall transpiration boundary condition and an edge velocity formula. The boundary layer edge velocity is expressed as a sum of the inviscid velocities and a correction dependent only on the boundary layer variables, determined by equations developed from the panel method calculation as a distribution of transpiration sources. These are superimposed on the body, including the lifting surfaces, as well as on the potential flow wakes. The boundary layer equations, with the global potential flow effects included via the transpiration source model, are solved by a full Newton's method. Numerical predictions for a sailing yacht hull are compared with experimental results obtained in a towing tank.</dim:field>
   <dim:field mdschema="dc" element="description" qualifier="statementofresponsibility" lang="en_US">by Claudio Cairoli.</dim:field>
   <dim:field mdschema="dc" element="description" qualifier="degree" lang="en_US">Ph.D.</dim:field>
   <dim:field mdschema="dc" element="format" qualifier="extent" lang="en_US">114 leaves</dim:field>
   <dim:field mdschema="dc" element="language" qualifier="iso" lang="en_US">eng</dim:field>
   <dim:field mdschema="dc" element="publisher" lang="en_US">Massachusetts Institute of Technology</dim:field>
   <dim:field mdschema="dc" element="rights" lang="en_US">M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission.</dim:field>
   <dim:field mdschema="dc" element="rights" qualifier="uri">http://dspace.mit.edu/handle/1721.1/7582</dim:field>
   <dim:field mdschema="dc" element="subject" lang="en_US">Mechanical Engineering.</dim:field>
   <dim:field mdschema="dc" element="title" lang="en_US">A theoretical and numerical procedure for predicting sailing yacht lift and drag</dim:field>
   <dim:field mdschema="dc" element="type" lang="en_US">Thesis</dim:field>
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   	&lt;Title>A theoretical and numerical procedure for predicting sailing yacht lift and drag&lt;/Title>
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   	&lt;PublicationDate>2007&lt;/PublicationDate>
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        	&lt;DisplayName>Cairoli, Claudio, 1975-&lt;/DisplayName>
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    &lt;Keyword>Mechanical Engineering.&lt;/Keyword>
   	&lt;Abstract&gt;In this thesis, a theoretical and numerical procedure for predicting the effects of viscosity on the hydrodynamic forces developed by a sailing yacht hull is presented. A simultaneous viscous/inviscid algorithm is developed by coupling a low order panel method with quasi three-dimensional integral boundary layer equations. A transom condition is used to prevent non-zero wave heights at the stern for a hull with overhangs. The influence of viscosity on the outer inviscid flow is modeled using a wall transpiration boundary condition and an edge velocity formula. The boundary layer edge velocity is expressed as a sum of the inviscid velocities and a correction dependent only on the boundary layer variables, determined by equations developed from the panel method calculation as a distribution of transpiration sources. These are superimposed on the body, including the lifting surfaces, as well as on the potential flow wakes. The boundary layer equations, with the global potential flow effects included via the transpiration source model, are solved by a full Newton&amp;apos;s method. Numerical predictions for a sailing yacht hull are compared with experimental results obtained in a towing tank.&lt;/Abstract>
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