<?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%">Toogood, T L</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">1568. Minimum and Maximum Cargo Tables for Aircraft With Three Cargo Compartments</style></title><secondary-title><style face="normal" font="default" size="100%">42nd Annual Conference, Anaheim, California, May 23-25</style></secondary-title></titles><keywords><keyword><style  face="normal" font="default" size="100%">02. Aircraft Loading - Payload</style></keyword></keywords><dates><year><style  face="normal" font="default" size="100%">1983</style></year><pub-dates><date><style  face="normal" font="default" size="100%">5/23/83</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=44055</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%">Anaheim, California</style></pub-location><pages><style face="normal" font="default" size="100%">11</style></pages><language><style face="normal" font="default" size="100%">eng</style></language><abstract><style face="normal" font="default" size="100%">This paper presents a procedure for calculating minimum and maximum cargo weights for aircraft with three cargo compartments. For a given number of passengers and a given amount of cargo, this procedure distributes the cargo load to each of three compartments in such a manner that the balance limits are never exceeded. A mathematical analysis is used to determine the intersection of the cargo vectors. One compartment is limited to a constant load by volume or structural limits while the quantities in the other two are determined.</style></abstract><work-type><style face="normal" font="default" size="100%">2. AIRCRAFT LOADING - PAYLOAD</style></work-type><accession-num><style face="normal" font="default" size="100%">1568</style></accession-num><custom1><style face="normal" font="default" size="100%">Non-Member Price: $10.00. 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><custom3><style face="normal" font="default" size="100%">10</style></custom3></record></records></xml>