{"title":"甲板发射乘波器配置飞机的概念设计","authors":"Conrad F. Newberry","doi":"10.1016/S1369-8869(98)00015-9","DOIUrl":null,"url":null,"abstract":"<div><p>The results of five graduate classroom design teams are reviewed in order to assess the feasibility of carriercapable tactical waverider-configured aircraft designed for cruise Mach numbers in the range 3≤<em>M</em><sub>∞</sub>≤5. The efforts of the design teams suggests that such aircraft are probably feasible for combat radii of <span><math><mtext>580</mtext><mspace></mspace><mtext>nm</mtext><mtext><R<1500</mtext><mspace></mspace><mtext>nm</mtext></math></span>. Low-speed research to support the development of such aircraft indicates that within the subsonic flight regime, waverider planforms may be statically unstable, vortex lift may be less strong for waverider configurations than for similar simple delta wing planforms and lift, drag and pitching moment data appear to be well behaved within a large (−20°≤<em>α</em>≤20° data shown herein) angle-of-attack range.</p></div>","PeriodicalId":100070,"journal":{"name":"Aircraft Design","volume":"1 3","pages":"Pages 159-191"},"PeriodicalIF":0.0000,"publicationDate":"1998-09-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"https://sci-hub-pdf.com/10.1016/S1369-8869(98)00015-9","citationCount":"3","resultStr":"{\"title\":\"The conceptual design of deck-launched waverider-configured aircraft\",\"authors\":\"Conrad F. Newberry\",\"doi\":\"10.1016/S1369-8869(98)00015-9\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><p>The results of five graduate classroom design teams are reviewed in order to assess the feasibility of carriercapable tactical waverider-configured aircraft designed for cruise Mach numbers in the range 3≤<em>M</em><sub>∞</sub>≤5. The efforts of the design teams suggests that such aircraft are probably feasible for combat radii of <span><math><mtext>580</mtext><mspace></mspace><mtext>nm</mtext><mtext><R<1500</mtext><mspace></mspace><mtext>nm</mtext></math></span>. Low-speed research to support the development of such aircraft indicates that within the subsonic flight regime, waverider planforms may be statically unstable, vortex lift may be less strong for waverider configurations than for similar simple delta wing planforms and lift, drag and pitching moment data appear to be well behaved within a large (−20°≤<em>α</em>≤20° data shown herein) angle-of-attack range.</p></div>\",\"PeriodicalId\":100070,\"journal\":{\"name\":\"Aircraft Design\",\"volume\":\"1 3\",\"pages\":\"Pages 159-191\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1998-09-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"https://sci-hub-pdf.com/10.1016/S1369-8869(98)00015-9\",\"citationCount\":\"3\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Aircraft Design\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S1369886998000159\",\"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/S1369886998000159","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
The conceptual design of deck-launched waverider-configured aircraft
The results of five graduate classroom design teams are reviewed in order to assess the feasibility of carriercapable tactical waverider-configured aircraft designed for cruise Mach numbers in the range 3≤M∞≤5. The efforts of the design teams suggests that such aircraft are probably feasible for combat radii of . Low-speed research to support the development of such aircraft indicates that within the subsonic flight regime, waverider planforms may be statically unstable, vortex lift may be less strong for waverider configurations than for similar simple delta wing planforms and lift, drag and pitching moment data appear to be well behaved within a large (−20°≤α≤20° data shown herein) angle-of-attack range.