{"title":"有或无弧度机翼的涡轮螺旋桨、涡扇或活塞螺旋桨飞机的航程和续航能力","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":"{\"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}","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}
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 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.
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