메뉴 건너뛰기




Volumn 1, Issue , 2007, Pages 396-420

A flexible hypersonic vehicle model developed with piston theory

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ALGORITHMS; HYPERSONIC AERODYNAMICS; MACH NUMBER; PISTONS; VEHICLES; COMPUTATION THEORY; GRAVITATION; MATHEMATICAL MODELS;

EID: 40549131567     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (92)

References (8)
  • 1
    • 0000458626 scopus 로고
    • Oscillating airfoils at high mach number
    • Lighthill, M., "Oscillating Airfoils at High Mach Number," Journal of the Aeronautical Sciences, Vol. 20, No. 6, 1953, pp. 402-406.
    • (1953) Journal of the Aeronautical Sciences , vol.20 , Issue.6 , pp. 402-406
    • Lighthill, M.1
  • 2
    • 0000051591 scopus 로고
    • Piston theory - A new aerodynamic tool for the aeroelastician
    • Ashley, H. and Zartarian, G., "Piston Theory - A New Aerodynamic Tool for the Aeroelastician," Journal of the Aeronautical Sciences, 1956, pp. 1109-1118.
    • (1956) Journal of the Aeronautical Sciences , pp. 1109-1118
    • Ashley, H.1    Zartarian, G.2
  • 3
    • 0029343262 scopus 로고
    • Stability derivatives for a hypersonic caret-wing waverider
    • Tarpley, C. and Lewis, M., "Stability Derivatives for a Hypersonic Caret-Wing Waverider," Journal of Aircraft, Vol. 32, No. 4, 1995, pp. 795-803.
    • (1995) Journal of Aircraft , vol.32 , Issue.4 , pp. 795-803
    • Tarpley, C.1    Lewis, M.2
  • 6


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.