<?xml version="1.0" encoding="UTF-8"?><xml><records><record><source-app name="Biblio" version="6.x">Drupal-Biblio</source-app><ref-type>47</ref-type><contributors><authors><author><style face="normal" font="default" size="100%">Schmidt, A H</style></author><author><style face="normal" font="default" size="100%">Dyess, S B</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">1926. Tilt Rotor Wing Weight Estimation</style></title><secondary-title><style face="normal" font="default" size="100%">49th Annual Conference, Chandler, Arizona, May 14-16</style></secondary-title></titles><keywords><keyword><style  face="normal" font="default" size="100%">23. Weight Engineering - Structural Estimation</style></keyword></keywords><dates><year><style  face="normal" font="default" size="100%">1990</style></year><pub-dates><date><style  face="normal" font="default" size="100%">5/14/90</style></date></pub-dates></dates><urls><web-urls><url><style face="normal" font="default" size="100%">http://www.sawe.org/store/product_info.php?products_id=39875</style></url></web-urls></urls><publisher><style face="normal" font="default" size="100%">Society of Allied Weight Engineers, Inc.</style></publisher><pub-location><style face="normal" font="default" size="100%">Chandler, Arizona</style></pub-location><pages><style face="normal" font="default" size="100%">34</style></pages><language><style face="normal" font="default" size="100%">eng</style></language><abstract><style face="normal" font="default" size="100%">The wing of a tilt rotor aircraft has some design requirements which differ from that of conventional aircraft.  The bending moment due to lifting the aircraft at the wing tips is larger than that of normal wing lift loads, and the natural frequency of the wing must be kept separated from the rotor one per rev.  This paper presents a method, based on composite construction, for tilt rotor wing weight estimation.</style></abstract><work-type><style face="normal" font="default" size="100%">23. WEIGHT ENGINEERING - STRUCTURAL ESTIMATION</style></work-type><accession-num><style face="normal" font="default" size="100%">1926</style></accession-num><custom1><style face="normal" font="default" size="100%">Non-Member Price: $21.42. Members may download this paper for free. &lt;a href=&quot;http://www.sawe.org/dms&quot;&gt;Click here&lt;/a&gt;. (Login Required. See SAWE &lt;a href=&quot;http://www.sawe.org/faq&quot;&gt;Frequently Asked Questions&lt;/a&gt;.)</style></custom1></record></records></xml>