<?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%">Lewis, L E</style></author><author><style face="normal" font="default" size="100%">St. John, R S</style></author></authors></contributors><titles><title><style face="normal" font="default" size="100%">1044. Allowable Stress Estimation Methods for Preliminary Design Weight Prediction</style></title><secondary-title><style face="normal" font="default" size="100%">34th Annual Conference, Seattle, Washington, May 5-7</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%">1975</style></year><pub-dates><date><style  face="normal" font="default" size="100%">5/5/75</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=40501</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%">Seattle, Washington</style></pub-location><pages><style face="normal" font="default" size="100%">57</style></pages><language><style face="normal" font="default" size="100%">eng</style></language><abstract><style face="normal" font="default" size="100%">This paper presents development of allowable stress estimation methods specifically tailored to
preliminary design weight prediction. The paper presents a unique analytical technique for projecting 
test results to cover a large variety of material/temperature combinations, including composite materials. 
It is shown how this approach overcomes inaccuracies and limitations associated with stress ratioing 
techniques by providing accountability for material strength limitations such as plasticity. Methods for 
compression, tension/fatigue and shear are developed.  Discussions are limited to primary wing, tail and
body structure. Method application examples are included in the paper. </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%">1044</style></accession-num><notes><style face="normal" font="default" size="100%">L. R. &quot;Mike&quot; Hackney Award</style></notes><custom1><style face="normal" font="default" size="100%">Non-Member Price: $35.91. 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>