Conceptual design of a third generation aerobatic aircraft

被引：3

作者：

Goraj, Zdobyslaw ^{[1
]}

Frydrychewicz, Andrzej ^{[2
]}

Danilecki, Stanislaw ^{[3
]}

Olejnik, Aleksander ^{[3
]}

Kiszkowiak, Lukasz ^{[3
]}

机构：

[1] Aircraft & Helicopter Design Dept, Nowowiejska 24, PL-00665 Warsaw, Poland

[2] Warsaw Univ Technol, Warsaw, Poland

[3] Mil Univ Technol, Fac Mechatron Armament & Aerosp, Warsaw, Poland

来源：

PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING | 2023年 / 237卷 / 07期

关键词：

aerobatic aircraft; aircraft design; permissible wing loading; safety of manoeuvres; performance in manoeuvres; DYNAMICS;

D O I：

10.1177/09544100221136327

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

This paper presents the development of an aerobatic aircraft including the influence of platform configuration on performance, elegance and safety of aerobatic manoeuvres. Several aircraft of different wing loadings were compared and the reduction of wing loading on manoeuvring slowdown was studied. Advantages of the biplane configuration influence on the desired properties of aerobatic aircraft were discussed in detail. Results of numerical simulations obtained for HARNAS-3 aircraft were compared with corresponding results received for EXTRA 300 aircraft. Some original design solutions for HARNAS-3, enabling easier control of this aircraft during the manoeuvring phase, were presented. Numerical simulations, wind tunnel tests and free flight experimental results for scaled-down HARNAS-3 models were presented, compared and discussed.

引用

页码：1696 / 1707

页数：12

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