Parametric study of a projectile launched by a compressed air cannon

Parametric study of a projectile launched by a compressed air cannon
  • Sung, Woojin; 
  • Kim, Jihoon; 
  • Jang, Kyeong sik; 
  • Le, Thi Thanh Giang; 
  • Kim, Jeonglae; 
  • ... Lee, Hyoungsoon; 
  • 외 2명
Citations

WEB OF SCIENCE

10
Citations

SCOPUS

11

초록

The principle of the compressed air cannon is that compressed air in the reservoir expands rapidly to propel the projectile. Previous studies assume that the tube pressure in front of the projectile is constant because the tube pressure was too low compared to the compressed air pressure in the reservoir. However, when the projectile actually travels in the tube, a compression wave is generated in front of the projectile. In this study, the theoretical prediction for the velocity of the projectile was performed using the tube pressure in front of the projectile affected by the compression wave as a variable. The results show that the maximum velocity decreases compared to previous studies. This difference from the constant tube pressure assumption cases becomes larger as the maximum velocity of the projectile increases. The theoretical prediction considering the compression wave shows a more realistic deceleration than when the tube pressure is constant. © 2023, The Korean Society of Mechanical Engineers and Springer-Verlag GmbH Germany, part of Springer Nature.

키워드

Compressible flow; Pressure wave; Projectile launch; Shock wave
제목
Parametric study of a projectile launched by a compressed air cannon
제목 (타언어)
Parametric study of a projectile launched by a compressed air cannon
저자
Sung, Woojin; Kim, Jihoon; Jang, Kyeong sik; Le, Thi Thanh Giang; Kim, Jeonglae; Kim, Dong Hyeon; Lee, Hyoungsoon; Ryu, Jaiyoung
DOI
10.1007/s12206-023-1029-x
발행일
2023-11
유형
Article
저널명
Journal of Mechanical Science and Technology
권
37
호
11
페이지
5913 ~ 5933