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Volumn , Issue , 2003, Pages

Sonic boom reduction through the use of non-axsymmetric configuration shaping

Author keywords

[No Author keywords available]

Indexed keywords


EID: 38849083315     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (7)

References (19)
  • 2
    • 84980073009 scopus 로고
    • The Flow Pattern of a Supersonic Projectile
    • Whitham, G.B., "The Flow Pattern of a Supersonic Projectile", Comm. Pure & Appl. Math, Vol. V, No. 3, 1952.
    • (1952) Comm. Pure & Appl. Math , vol.5 , Issue.3
    • Whitham, G.B.1
  • 3
    • 0008086929 scopus 로고
    • The Shock Pattern of a Wing-Body Combination, Far from the Flight Path
    • Walkden, F., "The Shock Pattern of a Wing-Body Combination, Far from the Flight Path", Aeronautical. Quarterly, Vol. 9, pg 164-194, 1958.
    • (1958) Aeronautical. Quarterly , vol.9 , pp. 164-194
    • Walkden, F.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.