https://www.scipedia.com/wd/index.php?action=history&feed=atom&title=Santos_et_al_2024a Santos et al 2024a - Revision history 2026-05-05T14:49:59Z Revision history for this page on the wiki MediaWiki 1.27.0-wmf.10 https://www.scipedia.com/wd/index.php?title=Santos_et_al_2024a&diff=305594&oldid=prev JSanchez: JSanchez moved page Draft Sanchez Pinedo 967971825 to Santos et al 2024a 2024-07-01T11:17:55Z <p>JSanchez moved page <a href="/public/Draft_Sanchez_Pinedo_967971825" class="mw-redirect" title="Draft Sanchez Pinedo 967971825">Draft Sanchez Pinedo 967971825</a> to <a href="/public/Santos_et_al_2024a" title="Santos et al 2024a">Santos et al 2024a</a></p> <table class="diff diff-contentalign-left" data-mw="interface"> <tr style='vertical-align: top;' lang='en'> <td colspan='1' style="background-color: white; color:black; text-align: center;">← Older revision</td> <td colspan='1' style="background-color: white; color:black; text-align: center;">Revision as of 11:17, 1 July 2024</td> </tr><tr><td colspan='2' style='text-align: center;' lang='en'><div class="mw-diff-empty">(No difference)</div> </td></tr></table> JSanchez https://www.scipedia.com/wd/index.php?title=Santos_et_al_2024a&diff=305593&oldid=prev JSanchez at 11:17, 1 July 2024 2024-07-01T11:17:49Z <p></p> <table class="diff diff-contentalign-left" data-mw="interface"> <col class='diff-marker' /> <col class='diff-content' /> <col class='diff-marker' /> <col class='diff-content' /> <tr style='vertical-align: top;' lang='en'> <td colspan='2' style="background-color: white; color:black; text-align: center;">← Older revision</td> <td colspan='2' style="background-color: white; color:black; text-align: center;">Revision as of 11:17, 1 July 2024</td> </tr><tr><td colspan="2" class="diff-lineno" id="mw-diff-left-l3" >Line 3:</td> <td colspan="2" class="diff-lineno">Line 3:</td></tr> <tr><td class='diff-marker'>&#160;</td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"></td><td class='diff-marker'>&#160;</td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"></td></tr> <tr><td class='diff-marker'>&#160;</td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"><div>This research project aims to investigate the mitigation of vibrations in the spars of aeronautical wings during flutter occurrences. The study will delve into aeroelastic phenomena, particularly focusing on flutter, defined as the self-excited interaction of vibration modes within a modified system, which can potentially lead to catastrophic failures. An analytical method has been developed to compute the flutter velocity, considering the stiffness and mass matrices, and the utilization of a Tuned Mass Damper (TMD) has been proposed to enhance the flutter velocity, thereby extending the aircraft's operational range. Suggestions for future research directions have been provided.</div></td><td class='diff-marker'>&#160;</td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"><div>This research project aims to investigate the mitigation of vibrations in the spars of aeronautical wings during flutter occurrences. The study will delve into aeroelastic phenomena, particularly focusing on flutter, defined as the self-excited interaction of vibration modes within a modified system, which can potentially lead to catastrophic failures. An analytical method has been developed to compute the flutter velocity, considering the stiffness and mass matrices, and the utilization of a Tuned Mass Damper (TMD) has been proposed to enhance the flutter velocity, thereby extending the aircraft's operational range. Suggestions for future research directions have been provided.</div></td></tr> <tr><td colspan="2">&#160;</td><td class='diff-marker'>+</td><td style="color:black; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div><ins style="font-weight: bold; text-decoration: none;"></ins></div></td></tr> <tr><td colspan="2">&#160;</td><td class='diff-marker'>+</td><td style="color:black; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div><ins style="font-weight: bold; text-decoration: none;">== Full Paper ==</ins></div></td></tr> <tr><td colspan="2">&#160;</td><td class='diff-marker'>+</td><td style="color:black; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div><ins style="font-weight: bold; text-decoration: none;">&lt;pdf&gt;Media:Draft_Sanchez Pinedo_967971825100.pdf&lt;/pdf&gt;</ins></div></td></tr> </table> JSanchez https://www.scipedia.com/wd/index.php?title=Santos_et_al_2024a&diff=305591&oldid=prev JSanchez at 11:17, 1 July 2024 2024-07-01T11:17:47Z <p></p> <table class="diff diff-contentalign-left" data-mw="interface"> <col class='diff-marker' /> <col class='diff-content' /> <col class='diff-marker' /> <col class='diff-content' /> <tr style='vertical-align: top;' lang='en'> <td colspan='2' style="background-color: white; color:black; text-align: center;">← Older revision</td> <td colspan='2' style="background-color: white; color:black; text-align: center;">Revision as of 11:17, 1 July 2024</td> </tr><tr><td colspan="2" class="diff-lineno" id="mw-diff-left-l1" >Line 1:</td> <td colspan="2" class="diff-lineno">Line 1:</td></tr> <tr><td colspan="2">&#160;</td><td class='diff-marker'>+</td><td style="color:black; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div><ins style="font-weight: bold; text-decoration: none;">&#160; &#160; &#160; &#160; &#160; &#160; &#160; &#160; &#160; &#160; &#160; &#160; &#160; &#160; &#160; &#160; </ins></div></td></tr> <tr><td colspan="2">&#160;</td><td class='diff-marker'>+</td><td style="color:black; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div><ins style="font-weight: bold; text-decoration: none;">==Abstract==</ins></div></td></tr> <tr><td class='diff-marker'>&#160;</td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"></td><td class='diff-marker'>&#160;</td><td style="background-color: #f9f9f9; color: #333333; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #e6e6e6; vertical-align: top; white-space: pre-wrap;"></td></tr> <tr><td colspan="2">&#160;</td><td class='diff-marker'>+</td><td style="color:black; font-size: 88%; border-style: solid; border-width: 1px 1px 1px 4px; border-radius: 0.33em; border-color: #a3d3ff; vertical-align: top; white-space: pre-wrap;"><div><ins style="font-weight: bold; text-decoration: none;">This research project aims to investigate the mitigation of vibrations in the spars of aeronautical wings during flutter occurrences. The study will delve into aeroelastic phenomena, particularly focusing on flutter, defined as the self-excited interaction of vibration modes within a modified system, which can potentially lead to catastrophic failures. An analytical method has been developed to compute the flutter velocity, considering the stiffness and mass matrices, and the utilization of a Tuned Mass Damper (TMD) has been proposed to enhance the flutter velocity, thereby extending the aircraft's operational range. Suggestions for future research directions have been provided.</ins></div></td></tr> </table> JSanchez https://www.scipedia.com/wd/index.php?title=Santos_et_al_2024a&diff=305590&oldid=prev JSanchez: Created blank page 2024-07-01T11:17:45Z <p>Created blank page</p> <p><b>New page</b></p><div></div> JSanchez