<?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%">Caddell, W E</style></author><author><style face="normal" font="default" size="100%">Karll, M P</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">982. A Computer-Aided Design Procedure to Approximate Aircraft Area Curve Shapes</style></title><secondary-title><style face="normal" font="default" size="100%">32nd Annual Conference, London, England, June 25-27</style></secondary-title></titles><keywords><keyword><style  face="normal" font="default" size="100%">12. Weight Engineering - Computer Applications</style></keyword></keywords><dates><year><style  face="normal" font="default" size="100%">1973</style></year><pub-dates><date><style  face="normal" font="default" size="100%">6/24/73</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=40581</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%">London, England</style></pub-location><pages><style face="normal" font="default" size="100%">13</style></pages><language><style face="normal" font="default" size="100%">eng</style></language><abstract><style face="normal" font="default" size="100%">A computerized math modeling routine providing approximation of Mach 1.0 aircraft area distribution has been developed to supplement and expedite the preliminary design process. This routine provides information that was heretofore considered to be impractical to produce with the frequency needed in design synthesis. This process is one of integrating dimensional characteristics of selectable components, comparing the results to a desired shape, and determining minimum practical body dimensions using configuration-dependent constraints. This process is of particular value to the mass properties engineer because of the interrelation between area curve shape and aircraft balance. </style></abstract><work-type><style face="normal" font="default" size="100%">12. WEIGHT ENGINEERING - COMPUTER APPLICATIONS</style></work-type><accession-num><style face="normal" font="default" size="100%">0982</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></record></records></xml>