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http://dx.doi.org/10.5139/JKSAS.2002.30.4.053

High Speed Wind Tunnel Test for the Rocket with Strap-on Boosters  

Ra, Seung-Ho (한국항공우주연구원 공력성능연구그룹)
Kim, In-Sun (한국항공우주연구원 공력성능연구그룹)
Choi, Seong-Wook (한국항공우주연구원 공력성능연구그룹)
Ok, Ho-Nam (한국항공우주연구원 공력성능연구그룹)
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.30, no.4, 2002 , pp. 53-63 More about this Journal
Abstract
The high speed wind tunnel test for the study of the basic aerodynamic characteristics of the rocket with twin strap-on boosters was performed using ADD trisonic wind tunnel on the Mach number range of 0.4~4.0. The 6 % scale model of the early design version of Korean sounding rocket was tested. The tested configurations were core only, core/fins, core/boosters and core/boosters/fins. The effects of core length, gap between core and booster, and bank angle were investigated.
Keywords
High Speed Wind Tunnel Test; Rocket; Booster; Compressible Flow;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
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