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Volumn 25, Issue 7, 1988, Pages 598-605

Efficient algorithm for solution of the unsteady transonic small-disturbance equation

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT--WINGS; FLOW OF FLUIDS--TRANSONIC; FLUID DYNAMICS--MATHEMATICAL MODELS;

EID: 0024038597     PISSN: 00218669     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.45629     Document Type: Article
Times cited : (55)

References (10)
  • 2
    • 0020205058 scopus 로고
    • Nonlinear Transonic Flutter Analysis
    • Nov
    • Borland C. J. and Rizzetta D. P. “Nonlinear Transonic Flutter Analysis” AIAA Journal Vol. 20 Nov. 1982 pp. 1606-1615.
    • (1982) AIAA Journal , vol.20 , pp. 1606-1615
    • Borland, C.J.1    Rizzetta, D.P.2
  • 3
    • 0022026464 scopus 로고
    • Efficient Algorithm for Unsteady Transonic Aerodynamics of Low-Aspect-Ratio Wings
    • March
    • Guruswamy G. P. and Goorjian P. M. “Efficient Algorithm for Unsteady Transonic Aerodynamics of Low-Aspect-Ratio Wings” Journal of Aircraft Vol. 22 March 1985 pp. 193-199.
    • (1985) Journal of Aircraft , vol.22 , pp. 193-199
    • Guruswamy, G.P.1    Goorjian, P.M.2
  • 5
    • 0023365807 scopus 로고
    • Calculation of Transonic Steady and Oscillatory Pressures on a Low Aspect Ratio Model
    • June
    • Bennett R. M. Wynne E. C. and Mabey D. G. “Calculation of Transonic Steady and Oscillatory Pressures on a Low Aspect Ratio Model” Journal of Aircraft Vol. 24 June 1987 pp. 392-398.
    • (1987) Journal of Aircraft , vol.24 , pp. 392-398
    • Bennett, R.M.1    Wynne, E.C.2    Mabey, D.G.3
  • 9
    • 85003277938 scopus 로고
    • Analysis of Embedded Shock Waves Calculated by Relaxation Methods
    • AIAA New York July
    • Murman E. M. “Analysis of Embedded Shock Waves Calculated by Relaxation Methods” Proceedings of AIAA Computational Fluid Dynamics Conference AIAA New York July 1973 pp. 27-40.
    • (1973) Proceedings of AIAA Computational Fluid Dynamics Conference , pp. 27-40
    • Murman, E.M.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.