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Volumn 23, Issue 5, 2000, Pages 922-929

Computational test cases for the benchmark active controls model

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEM ANALYSIS; CONTROL SYSTEM SYNTHESIS; DEFLECTION (STRUCTURES); MATHEMATICAL MODELS; OSCILLATIONS;

EID: 0034274437     PISSN: 07315090     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.4634     Document Type: Article
Times cited : (35)

References (37)
  • 6
    • 0029219120 scopus 로고
    • Summary of an active flexible wing program
    • Perry, B., III, Cole, S. R., and Miller, G. D., "Summary of an Active Flexible Wing Program," Journal of Aircraft, Vol. 32, No. 1, 1995, pp. 10-15.
    • (1995) Journal of Aircraft , vol.32 , Issue.1 , pp. 10-15
    • Perry B. III1    Cole, S.R.2    Miller, G.D.3
  • 9
    • 0034275786 scopus 로고    scopus 로고
    • Scott, R. C., Hoadley, S. T., Wieseman, C. D., and Durham, M. H., "Benchmark Active Controls Technology Model Aerodynamic Data," AIAA Paper 97-0829, Jan. 1997; also Journal of Guidance, Control, and Dynamics, Vol. 23, No. 5, 2000, pp. 914-921.
    • (2000) Journal of Guidance, Control, and Dynamics , vol.23 , Issue.5 , pp. 914-921
  • 10
    • 0003832391 scopus 로고
    • Compendium of unsteady aerodynamic measurements
    • Aug.
    • "Compendium of Unsteady Aerodynamic Measurements," AGARD Rept. 702, Aug. 1982.
    • (1982) AGARD Rept. 702
  • 11
    • 0343736761 scopus 로고
    • Compendium of unsteady aerodynamic measurements, addendum no. 1
    • May
    • "Compendium of Unsteady Aerodynamic Measurements, Addendum No. 1," AGARD Rept. 702, May 1985.
    • (1985) AGARD Rept. 702
  • 13
    • 84964237806 scopus 로고    scopus 로고
    • Comparison of two Navier-Stokes aeroelastic methods using BACT benchmark experimental data
    • to be published
    • Bartels, R. E., and Schuster, D. M., "Comparison of Two Navier-Stokes Aeroelastic Methods Using BACT Benchmark Experimental Data," Journal of Guidance, Control, and Dynamics (to be published).
    • Journal of Guidance, Control, and Dynamics
    • Bartels, R.E.1    Schuster, D.M.2
  • 23
    • 0010361384 scopus 로고
    • Aeroelasticity Branch, NASA Langley Research Center, LWP-799, Hampton, VA, Sept.
    • "The Langley Transonic Dynamics Tunnel," Aeroelasticity Branch, NASA Langley Research Center, LWP-799, Hampton, VA, Sept. 1969.
    • (1969) The Langley Transonic Dynamics Tunnel


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.