Approximate solutions of range for constant altitude - constant high subsonic speed flight of transport aircraft

被引：13

作者：

Cavcar, A ^{[1
]}

Cavcar, M ^{[1
]}

机构：

[1] Anadolu Univ, Sch Civil Aviat, Eskisehir, Turkey

来源：

AEROSPACE SCIENCE AND TECHNOLOGY | 2004年 / 8卷 / 06期

关键词：

aircraft range; aircraft performance; optimum cruise speed; preliminary design;

D O I：

10.1016/j.ast.2004.04.002

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Approximate cruise range solutions are introduced for the constant altitude - constant high subsonic speed flight of turbojet/fan transport aircraft with cambered wing design. The variation of the specific fuel consumption with Mach number is also considered in derivation of the approximate solutions. The method aims at estimation of the cruise range of aircraft during conceptual or preliminary design phase. An application of the solutions is also presented. (C) 2004 Elsevier SAS. All rights reserved.

引用

页码：557 / 567

页数：11

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