<?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%">Peterson, Dr. , P W</style></author><author><style face="normal" font="default" size="100%">Reidinger, L A</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">185. Weight Savings in the Presence of Thermal Stresses</style></title><secondary-title><style face="normal" font="default" size="100%">17th Annual Conference, Belmont Plaza Hotel, New York, New York, May 19-22</style></secondary-title></titles><keywords><keyword><style  face="normal" font="default" size="100%">22. Weight Engineering - Structural Design</style></keyword></keywords><dates><year><style  face="normal" font="default" size="100%">1958</style></year><pub-dates><date><style  face="normal" font="default" size="100%">5/19/58</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=44965</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%">New York, New York</style></pub-location><pages><style face="normal" font="default" size="100%">16</style></pages><language><style face="normal" font="default" size="100%">eng</style></language><abstract><style face="normal" font="default" size="100%">In designing structures for flight vehicles which must operate in high temperature environments, it is necessary to choose materials which will withstand thermal stresses in addition to normal load factors.  In analyzing for optimum material combinations, the weight advantages or penalties which may accrue must also be taken into account. In this paper, a method is presented for selecting material combinations which result in low thermal stresses and reduce structural weight to a minimum. Two example problems are given. </style></abstract><work-type><style face="normal" font="default" size="100%">22. WEIGHT ENGINEERING - STRUCTURAL DESIGN</style></work-type><accession-num><style face="normal" font="default" size="100%">0185</style></accession-num><custom1><style face="normal" font="default" size="100%">Non-Member Price: $10.08. 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%">10.08</style></custom3></record></records></xml>