Aerodynamic and stability analysis of personal vehicle in tandem-wing configuration

被引：14
|
作者：
Goetzendorf-Grabowski, Tomasz [1 ]
Figat, Marcin [1 ]
机构：
[1] Warsaw Univ Technol, Fac Power & Aeronaut Engn, Nowowiejska 24, PL-00665 Warsaw, Poland
来源：
PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING | 2017年 / 231卷 / 11期
关键词：
Aircraft design; personal air transport systems; tandem wing; stability; flying qualities; aerodynamics;
D O I：
10.1177/0954410016662077
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
The paper presents a concept of tandem-wing configuration aircraft that was a Warsaw University of Technology proposal for the personal air transport system. The project was developed at Warsaw University of Technology, within the PPLANE project (FP7 - Personal Plane: Assessment and Validation of Pioneering Concepts for Personal Air Transport Systems). First, analysis of the general concept, advantages and disadvantages of tandem-wing configuration, and possible application as a personal air transport system vehicle are presented. Next, aerodynamic design is analyzed and dynamic stability is tested. All numerical analyses were made by use of the well-tested professional software for aerodynamic (MGAERO) and stability (SDSA) analyses.
引用
收藏
页码：2146 / 2162
页数：17
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