메뉴 건너뛰기




Volumn 39, Issue 8, 2001, Pages 1553-1561

Chapman-Jouguet oblique detonation structure around hypersonic projectiles

Author keywords

[No Author keywords available]

Indexed keywords

CAMERAS; CHARGE COUPLED DEVICES; DETONATION; PRESSURE EFFECTS; PROJECTILES; SHOCK WAVES; WAVE PROPAGATION; WAVEFRONTS;

EID: 0035421050     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.1480     Document Type: Article
Times cited : (50)

References (27)
  • 6
    • 0001462057 scopus 로고    scopus 로고
    • Prediction method of unsteady combustion around hypersonic projectile in stoichiometric hydrogen-air
    • (1998) AIAA Journal , vol.36 , Issue.10 , pp. 1834-1841
    • Matsuo, A.1    Fujii, K.2
  • 7
    • 0001140571 scopus 로고    scopus 로고
    • Detailed mechanism of the unsteady combustion around hypersonic projectiles
    • (1996) AIAA Journal , vol.34 , Issue.10 , pp. 2082-2089
    • Matsuo, A.1    Fujii, K.2
  • 12
    • 0004180160 scopus 로고    scopus 로고
    • The effect of confinement on detonation initiation by blunt projectiles
    • July
    • (1997) AIAA Paper , vol.97 , Issue.3179
    • Higgins, A.J.1
  • 22
    • 0003792892 scopus 로고
    • Oblique detonations: Theory and propulsion applications
    • edited by J. Buckmaster, T. L. Jackson, and A. Kumar, Kluwer Academic, The Netherlands
    • (1994) Combustion in High-Speed Flows , pp. 345-371
    • Powers, J.M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.