Range and endurance of turboprop, turbofan, or piston–propeller aircraft having wings with or without camber

New analytic expressions, based on the exact performance relationships without making the approximations on which the classical Breguel equation is based, are developed to predict cruising range and endurance of turboprop, turbofan, or piston-propeller aircraft at constant speed and altitude. Also,...

Full description

Saved in:
Bibliographic Details
Published in:Aircraft design : an international journal 1999-12, Vol.2 (4), p.183-190
Main Author: Bert, Charles W
Format: Article
Language:English
Citations: Items that this one cites
Items that cite this one
Online Access:Get full text
Tags: Add Tag
No Tags, Be the first to tag this record!
cited_by cdi_FETCH-LOGICAL-c197t-20001aa19d6b04786320fc70e5fe356f7c8fa75486ced6bb8f03539fe823e1af3
cites cdi_FETCH-LOGICAL-c197t-20001aa19d6b04786320fc70e5fe356f7c8fa75486ced6bb8f03539fe823e1af3
container_end_page 190
container_issue 4
container_start_page 183
container_title Aircraft design : an international journal
container_volume 2
creator Bert, Charles W
description New analytic expressions, based on the exact performance relationships without making the approximations on which the classical Breguel equation is based, are developed to predict cruising range and endurance of turboprop, turbofan, or piston-propeller aircraft at constant speed and altitude. Also, the optimal cruising speed to achieve maximum range is determined. (Author)
doi_str_mv 10.1016/S1369-8869(99)00013-0
format article
fullrecord <record><control><sourceid>proquest_cross</sourceid><recordid>TN_cdi_proquest_miscellaneous_27102050</recordid><sourceformat>XML</sourceformat><sourcesystem>PC</sourcesystem><sourcerecordid>27102050</sourcerecordid><originalsourceid>FETCH-LOGICAL-c197t-20001aa19d6b04786320fc70e5fe356f7c8fa75486ced6bb8f03539fe823e1af3</originalsourceid><addsrcrecordid>eNo9UMtOwzAQ9AEkSuETkHxCIDWwjhsnPqKKl1QJicfZctx1G9TawU5A3PgH_pAvwWkRl5nV7OxqNIScMLhgwMTlE-NCZlUl5JmU5wDAeAZ7ZPQvH5DDGF-TnpeVGBH3qN0SqXYLim7RB-0MUm9p14fat8G3k91otZtQH2jbxM67n6_vYYfrNQaqm2CCth1d6ffGLelHgpiwWw0HA_u-o0ZvagxHZN_qdcTjPx6Tl5vr59ldNn-4vZ9dzTPDZNll-RBcayYXooZpCspzsKYELCzyQtjSVFaXxbQSBpOlrizwgkuLVc6RacvH5HT3N8V86zF2atNEk_Jqh76PKi8Z5FBAMhY7owk-xoBWtaHZ6PCpGKihUbVtVA3VKSnVtlEF_BcKI26j</addsrcrecordid><sourcetype>Aggregation Database</sourcetype><iscdi>true</iscdi><recordtype>article</recordtype><pqid>27102050</pqid></control><display><type>article</type><title>Range and endurance of turboprop, turbofan, or piston–propeller aircraft having wings with or without camber</title><source>ScienceDirect Freedom Collection</source><creator>Bert, Charles W</creator><creatorcontrib>Bert, Charles W</creatorcontrib><description>New analytic expressions, based on the exact performance relationships without making the approximations on which the classical Breguel equation is based, are developed to predict cruising range and endurance of turboprop, turbofan, or piston-propeller aircraft at constant speed and altitude. Also, the optimal cruising speed to achieve maximum range is determined. (Author)</description><identifier>ISSN: 1369-8869</identifier><identifier>DOI: 10.1016/S1369-8869(99)00013-0</identifier><language>eng</language><ispartof>Aircraft design : an international journal, 1999-12, Vol.2 (4), p.183-190</ispartof><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c197t-20001aa19d6b04786320fc70e5fe356f7c8fa75486ced6bb8f03539fe823e1af3</citedby><cites>FETCH-LOGICAL-c197t-20001aa19d6b04786320fc70e5fe356f7c8fa75486ced6bb8f03539fe823e1af3</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><link.rule.ids>314,780,784,27923,27924</link.rule.ids></links><search><creatorcontrib>Bert, Charles W</creatorcontrib><title>Range and endurance of turboprop, turbofan, or piston–propeller aircraft having wings with or without camber</title><title>Aircraft design : an international journal</title><description>New analytic expressions, based on the exact performance relationships without making the approximations on which the classical Breguel equation is based, are developed to predict cruising range and endurance of turboprop, turbofan, or piston-propeller aircraft at constant speed and altitude. Also, the optimal cruising speed to achieve maximum range is determined. (Author)</description><issn>1369-8869</issn><fulltext>true</fulltext><rsrctype>article</rsrctype><creationdate>1999</creationdate><recordtype>article</recordtype><recordid>eNo9UMtOwzAQ9AEkSuETkHxCIDWwjhsnPqKKl1QJicfZctx1G9TawU5A3PgH_pAvwWkRl5nV7OxqNIScMLhgwMTlE-NCZlUl5JmU5wDAeAZ7ZPQvH5DDGF-TnpeVGBH3qN0SqXYLim7RB-0MUm9p14fat8G3k91otZtQH2jbxM67n6_vYYfrNQaqm2CCth1d6ffGLelHgpiwWw0HA_u-o0ZvagxHZN_qdcTjPx6Tl5vr59ldNn-4vZ9dzTPDZNll-RBcayYXooZpCspzsKYELCzyQtjSVFaXxbQSBpOlrizwgkuLVc6RacvH5HT3N8V86zF2atNEk_Jqh76PKi8Z5FBAMhY7owk-xoBWtaHZ6PCpGKihUbVtVA3VKSnVtlEF_BcKI26j</recordid><startdate>19991201</startdate><enddate>19991201</enddate><creator>Bert, Charles W</creator><scope>AAYXX</scope><scope>CITATION</scope><scope>7TB</scope><scope>8FD</scope><scope>FR3</scope><scope>H8D</scope><scope>KR7</scope><scope>L7M</scope></search><sort><creationdate>19991201</creationdate><title>Range and endurance of turboprop, turbofan, or piston–propeller aircraft having wings with or without camber</title><author>Bert, Charles W</author></sort><facets><frbrtype>5</frbrtype><frbrgroupid>cdi_FETCH-LOGICAL-c197t-20001aa19d6b04786320fc70e5fe356f7c8fa75486ced6bb8f03539fe823e1af3</frbrgroupid><rsrctype>articles</rsrctype><prefilter>articles</prefilter><language>eng</language><creationdate>1999</creationdate><toplevel>peer_reviewed</toplevel><toplevel>online_resources</toplevel><creatorcontrib>Bert, Charles W</creatorcontrib><collection>CrossRef</collection><collection>Mechanical &amp; Transportation Engineering Abstracts</collection><collection>Technology Research Database</collection><collection>Engineering Research Database</collection><collection>Aerospace Database</collection><collection>Civil Engineering Abstracts</collection><collection>Advanced Technologies Database with Aerospace</collection><jtitle>Aircraft design : an international journal</jtitle></facets><delivery><delcategory>Remote Search Resource</delcategory><fulltext>fulltext</fulltext></delivery><addata><au>Bert, Charles W</au><format>journal</format><genre>article</genre><ristype>JOUR</ristype><atitle>Range and endurance of turboprop, turbofan, or piston–propeller aircraft having wings with or without camber</atitle><jtitle>Aircraft design : an international journal</jtitle><date>1999-12-01</date><risdate>1999</risdate><volume>2</volume><issue>4</issue><spage>183</spage><epage>190</epage><pages>183-190</pages><issn>1369-8869</issn><abstract>New analytic expressions, based on the exact performance relationships without making the approximations on which the classical Breguel equation is based, are developed to predict cruising range and endurance of turboprop, turbofan, or piston-propeller aircraft at constant speed and altitude. Also, the optimal cruising speed to achieve maximum range is determined. (Author)</abstract><doi>10.1016/S1369-8869(99)00013-0</doi><tpages>8</tpages></addata></record>
fulltext fulltext
identifier ISSN: 1369-8869
ispartof Aircraft design : an international journal, 1999-12, Vol.2 (4), p.183-190
issn 1369-8869
language eng
recordid cdi_proquest_miscellaneous_27102050
source ScienceDirect Freedom Collection
title Range and endurance of turboprop, turbofan, or piston–propeller aircraft having wings with or without camber
url http://sfxeu10.hosted.exlibrisgroup.com/loughborough?ctx_ver=Z39.88-2004&ctx_enc=info:ofi/enc:UTF-8&ctx_tim=2025-01-13T03%3A59%3A28IST&url_ver=Z39.88-2004&url_ctx_fmt=infofi/fmt:kev:mtx:ctx&rfr_id=info:sid/primo.exlibrisgroup.com:primo3-Article-proquest_cross&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.genre=article&rft.atitle=Range%20and%20endurance%20of%20turboprop,%20turbofan,%20or%20piston%E2%80%93propeller%20aircraft%20having%20wings%20with%20or%20without%20camber&rft.jtitle=Aircraft%20design%20:%20an%20international%20journal&rft.au=Bert,%20Charles%20W&rft.date=1999-12-01&rft.volume=2&rft.issue=4&rft.spage=183&rft.epage=190&rft.pages=183-190&rft.issn=1369-8869&rft_id=info:doi/10.1016/S1369-8869(99)00013-0&rft_dat=%3Cproquest_cross%3E27102050%3C/proquest_cross%3E%3Cgrp_id%3Ecdi_FETCH-LOGICAL-c197t-20001aa19d6b04786320fc70e5fe356f7c8fa75486ced6bb8f03539fe823e1af3%3C/grp_id%3E%3Coa%3E%3C/oa%3E%3Curl%3E%3C/url%3E&rft_id=info:oai/&rft_pqid=27102050&rft_id=info:pmid/&rfr_iscdi=true