Application of Integrated Layout for ”Cryogenic“ Transport Category Aircraft

被引：0
|
作者：
Kretov A.S. [1 ]
Glukhov V.V. [2 ]
机构：
[1] Nanjing University of Aeronautics and Astronautics, 29 Yudao St., Nanjing
[2] Gorbunov Kazan Aviation Plant, branch of PAO Tupolev, ul. Dement’eva 1, Tatarstan, Kazan
来源：
Russian Aeronautics | 2022年 / 65卷 / 1期
关键词：
blended wing body scheme; cryogenic fuel; fuel efficiency; numerical analysis; sensitivity factor of airplane take-off mass;
D O I：
10.3103/S1068799822010020
中图分类号：
学科分类号：
摘要：
Abstract: Based on the analysis of the sensitivity of mass to the initial change of parameters, an assessment is made of the transition from the traditional layout of a transport category aircraft to the blended wing body scheme followed by the transition to cryogenic fuels. As an example, a passenger airplane for 450–500 passengers with a range of 10,000 km is considered. A comparative analysis of the mass and fuel efficiency of the considered schemes is given. © 2022, Allerton Press, Inc.
引用
收藏
页码：10 / 24
页数：14
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