제어로봇시스템학회:학술대회논문집
- 1988.10a
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- Pages.608-613
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- 1988
Experimental study on aerodynamic characteristics of launcher at subsonic speed
아음속 유동에서의 발사체의 공력특성에 관한 실험 연구
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.
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