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Volumn , Issue , 1997, Pages

An unsteady simulation technique for missile guidance and control applications

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; AIR NAVIGATION; APPLICATION PROGRAMS; COMPUTATIONAL FLUID DYNAMICS; ELECTRONIC GUIDANCE SYSTEMS; FINS (HEAT EXCHANGE); MISSILES; VERTICAL STABILIZERS;

EID: 84983168908     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (7)

References (6)
  • 5
    • 0028466644 scopus 로고    scopus 로고
    • Time-Accurate Computational Fluid Dynamics Approach to Transonic Store Separation Trajectory Prediction
    • Lijewski, L.E., Suhs, N.E., " Time-Accurate Computational Fluid Dynamics Approach to Transonic Store Separation Trajectory Prediction", Journal of Aircraft, Volume 31, № 4, Pages 886-891.
    • Journal of Aircraft , vol.31 , Issue.4 , pp. 886-891
    • Lijewski, L.E.1    Suhs, N.E.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.