<?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></authors></contributors><titles><title><style face="normal" font="default" size="100%">1162. Design Considerations in Formulating V/STOL Lift Plus Lift/Cruise Supersonic Fighter Concepts</style></title><secondary-title><style face="normal" font="default" size="100%">36th Annual Conference, San Diego, California, May 9-12</style></secondary-title></titles><keywords><keyword><style  face="normal" font="default" size="100%">30. Miscellaneous</style></keyword></keywords><dates><year><style  face="normal" font="default" size="100%">1977</style></year><pub-dates><date><style  face="normal" font="default" size="100%">5/9/77</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=40425</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%">San Diego, California</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%">Several means of providing V/STOL thrust are examined and discussed relative to their impact on the design of supersonic fighters.  The lift plus lift/cruise concept is discussed in more detail, specifically addressing both the advantages and concerns that exist with that system. The principal concern is the operational footprint (temperature and noise).  The principal advantage is its minimal impact on airframe design, aerodynamic parameters, and fuel requirements, which are the major parameters in weight growth spiral effects.  The conclusion is that lift plus lift/cruise advances result from differences that are fundamental, and that this concept will generally result in the lightest weight and lowest cost supersonic fighter designed to a specific operational requirement.</style></abstract><work-type><style face="normal" font="default" size="100%">30. MISCELLANEOUS</style></work-type><accession-num><style face="normal" font="default" size="100%">1162</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>