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Volumn , Issue , 2000, Pages

Steady-state computation of constant rotational rate dynamic stability derivatives

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRCRAFT; COMPUTATIONAL FLUID DYNAMICS; COMPUTATIONAL METHODS; STABILITY; WIND TUNNELS;

EID: 85088184528     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-4321     Document Type: Conference Paper
Times cited : (36)

References (16)
  • 1
    • 0003595356 scopus 로고    scopus 로고
    • Manual (Version 5.0)NASA TM-1998-20844, June
    • Krist, E., Biedron, R., and Rumsey, C., "CFL3D User's Manual (Version 5.0)" NASA TM-1998-20844, June 1998.
    • (1998) CFL3D User's
    • Krist, E.1    Biedron, R.2    Rumsey, C.3
  • 3
    • 33745007240 scopus 로고
    • Unsteady Vortex-Dominated Flows around Maneuvering Wings over a wide Range of Mach Numbers
    • Jan
    • Kandil, O. A., and Chuang, H. A., "Unsteady Vortex-Dominated Flows around Maneuvering Wings over a wide Range of Mach Numbers," AIAA Paper 88-0317, Jan. 1988.
    • (1988) AIAA Paper , pp. 88-0317
    • Kandil, O.A.1    Chuang, H.A.2
  • 4
    • 0025489132 scopus 로고
    • Unsteady Navier-Stokes Computations Past Oscillating Delta Wing at High Incidence
    • Sept
    • Kandil, O. A., and Chuang, H. A., "Unsteady Navier-Stokes Computations Past Oscillating Delta Wing at High Incidence," AIAA Journal, Vol. 28, No. 9, Sept. 1990, pp. 1565-1572.
    • (1990) AIAA Journal , vol.28 , Issue.9 , pp. 1565-1572
    • Kandil, O.A.1    Chuang, H.A.2
  • 11
    • 0041717411 scopus 로고    scopus 로고
    • Department of Computational and Applied Mathematics, Rice University, CAAM-TR 00-02, Jan
    • Carle, A. and Fagan, M., "Overview of Adifor 3.0," Department of Computational and Applied Mathematics, Rice University, CAAM-TR 00-02, Jan. 2000.
    • (2000) Overview of Adifor 3.0
    • Carle, A.1    Fagan, M.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.