DOI QR코드

DOI QR Code

The Vertical Wind Tunnel Test for Spin Mode Improvement of KTX-1

훈련기 스핀모드 향상을 위한 수직 풍동시험

  • Published : 2005.03.01

Abstract

This paper presents the efforts of the studies for improvement of spin characteristics of KTX-1 #02 through rotary balance test, forced oscillation test and spin mode analysis. During the full scale development design stage, we had fullfilled a lot of spin flight test, spin mode analysis. Based on all of the efforts, KTX-1 had been developed as a successful trainer with excellent spin characteristics.

Keywords

References

  1. V. Mansart, M. G., 'Spin study on KTX-1 model provisory report', ONERA-IMFL, 1990, 4
  2. 'Military specification-flying qualities of piloted aircraft', Mil-F-8785, November 1980
  3. M. Goman, A. Khramtsovsky, V. Soukhanov, et al. 'Aircraft spin prevention/recovery control system' 3-rd Russian-Chinese Conference on Aerodynamics and Flight Dynamics, TsAGI, Russia, November 1993
  4. William Bihrle, Jr. and Bamhart 'Spin prediction techniques', Journal of Aircraft, vol. 20, November 2, February 1983 https://doi.org/10.2514/3.44837
  5. 고준수외 5명, '훈련지원기 KTX-1의 초도 스핀 시험결과 분석', 제2회 항공기 개발 기술 Symposium, September 27, 1994