Conceptual design of a third generation aerobatic aircraft-Reference-Cited by-同舟云学术

Conceptual design of a third generation aerobatic aircraft

Published:2022-11-04 Issue: Volume: Page:095441002211363
ISSN:0954-4100
Container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
language:en
Short-container-title:Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering

Author:

Goraj Zdobyslaw¹^ORCID,Frydrychewicz Andrzej²,Danilecki Stanislaw³,Olejnik Aleksander³,Kiszkowiak Łukasz³^ORCID

Affiliation:

1. Aircraft and Helicopter Design Department, Warsaw, Poland

2. Warsaw University of Technology, Warsaw, Poland

3. Faculty of Mechatronics, Armament and Aerospace, Military University of Technology, Warsaw, Poland

Abstract

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.

Publisher

SAGE Publications

Subject

Mechanical Engineering,Aerospace Engineering

Link

http://journals.sagepub.com/doi/pdf/10.1177/09544100221136327

Reference20 articles.

1. Kalpas R, Solak B. Aerobatics (in polish: akrobatyka lotnicza. Książnica polska). Glasgow, 1945.

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