Design and Simulation of Ring-Slot Type Brake Parachute

被引：0
|
作者：
Jain A. [1 ]
Kandikonda H.R. [1 ]
Saxena A.K. [2 ]
机构：
[1] Dayalbagh Educational Institute, Uttar Pradesh, Agra
[2] DRDO - Aerial Delivery Research and Development Establishment, Agra
来源：
Journal of The Institution of Engineers (India): Series C | 2022年 / 103卷 / 04期
关键词：
Brake parachute; Design and simulation; Light weight aircraft;
D O I：
10.1007/s40032-022-00826-8
中图分类号：
学科分类号：
摘要：
Brake parachutes play an important role in aircraft landings as they are designed to slow down the speed of an aircraft. The brake parachutes are effective, especially for landing on the slippery surface during the regular and emergency landings of the aircraft. In this paper, an algorithm is developed to design a ring-slot type brake parachute based on deployment speed and required dynamic characteristics. A computational model is developed using MATLAB to simulate the behaviour of the canopy of ring-slot type brake parachute during inflation and after inflation. The methodology is explained through a case study of designing a ring-slot type brake parachute for a light weight aircraft in the range of 900–26000 kg. © 2022, The Institution of Engineers (India).
引用
收藏
页码：717 / 731
页数：14
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