Experimental study on aerodynamic characteristics of launcher at subsonic speed

아음속 유동에서의 발사체의 공력특성에 관한 실험 연구

  • 노오현 (서울대학교 항공공학과) ;
  • 이동호 (서울대학교 항공공학과) ;
  • 김원욱 (서울대학교 항공공학과) ;
  • 김철완 (서울대학교 항공공학과)
  • Published : 1988.10.01

Abstract

Subsonic aerodynamic force and moment characteristics have been determined for parametric groups of launchers. Geometric variables considered in the experimental study were body length, nose planform, fin planform (body-alone contained), number of stage and existence of extrnal booster, All data were obtained for angles of attack from 0 to 27 deg in 3-deg. increments.

Keywords