<?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%">Author, No</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">163. A Study to Promote Weight Control of Items Designed to Airframe Manufacturers Specifications</style></title><secondary-title><style face="normal" font="default" size="100%">16th National Conference, Broadview Hotel, Wichita, Kansas, April 29 - May 2</style></secondary-title></titles><keywords><keyword><style  face="normal" font="default" size="100%">10. Weight Engineering - Aircraft Design</style></keyword></keywords><dates><year><style  face="normal" font="default" size="100%">1957</style></year><pub-dates><date><style  face="normal" font="default" size="100%">5/29/57</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=41138</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%">Wichita, Kansas</style></pub-location><pages><style face="normal" font="default" size="100%">18</style></pages><language><style face="normal" font="default" size="100%">eng</style></language><abstract><style face="normal" font="default" size="100%">The Special Projects Committee of the St. Louis Chapter, S.A.W.E. undertook to determine the present state of the art concerning weight control on items designed by vendors to airframe manufacturers specifications.  This was accomplished by a survey questionnaire that was sent to 125 vendors and 50 airframe manufacturers.  With the present trend toward the weapons system design concept and the consequent large percentage of the design work of a project being done by vendors, the need for a unified approach to the problem of weight control becomes critically evident. </style></abstract><work-type><style face="normal" font="default" size="100%">10. WEIGHT ENGINEERING - AIRCRAFT DESIGN</style></work-type><accession-num><style face="normal" font="default" size="100%">0163</style></accession-num><custom1><style face="normal" font="default" size="100%">Non-Member Price: $11.34. 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>