{"title":"Range and endurance of turboprop, turbofan, or piston–propeller aircraft having wings with or without camber","authors":"Charles W Bert","doi":"10.1016/S1369-8869(99)00013-0","DOIUrl":null,"url":null,"abstract":"<div><p>New analytic expressions, based on the exact performance relationships without making the approximations on which the classical Breguet 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.</p></div>","PeriodicalId":100070,"journal":{"name":"Aircraft Design","volume":"2 4","pages":"Pages 183-190"},"PeriodicalIF":0.0000,"publicationDate":"1999-12-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.1016/S1369-8869(99)00013-0","citationCount":"16","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"Aircraft Design","FirstCategoryId":"1085","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S1369886999000130","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 16
Abstract
New analytic expressions, based on the exact performance relationships without making the approximations on which the classical Breguet 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.
京公网安备 11010802042870号
京ICP备2023020795号-1
分享
求助内容：
应助结果提醒方式：
扫码关注我们
