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Volumn 5, Issue , 2007, Pages 5247-5262

Active aeroelastic control over a multi-surface wing: Modelling and wind tunnel testing

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; BENDING (DEFORMATION); MATHEMATICAL MODELS; MODAL ANALYSIS; OPTIMIZATION; TUNNELS;

EID: 34547529746     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2007-2138     Document Type: Conference Paper
Times cited : (6)

References (19)
  • 1
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    • Reduction of structural loads using maneuver load control on the advanced fighter technology integration (AFTI) mission adaptive wing
    • NASA
    • Thornton, S. V., "Reduction of structural loads using maneuver load control on the advanced fighter technology integration (AFTI) mission adaptive wing," Tm 4526, NASA, 1993.
    • (1993) Tm 4526
    • Thornton, S.V.1
  • 2
    • 0035472772 scopus 로고    scopus 로고
    • Adaptive wing and flow control technology
    • Stanewsky, E., "Adaptive wing and flow control technology," Progress in Aerospace Sciences, Vol. 37, 2001, pp. 583667.
    • (2001) Progress in Aerospace Sciences , vol.37 , pp. 583667
    • Stanewsky, E.1
  • 5
    • 2042544288 scopus 로고    scopus 로고
    • Development and Application of an Optimization Procedure for Flutter Suppression Using the Aerodynamic Energy Concept
    • NASA
    • Nissim, E. and Abel, I., "Development and Application of an Optimization Procedure for Flutter Suppression Using the Aerodynamic Energy Concept," TP 1137, NASA.
    • TP 1137
    • Nissim, E.1    Abel, I.2
  • 10
    • 0034226416 scopus 로고    scopus 로고
    • Active Aeroelastic Wing Flight Research Program: Technical Program and Model Analytical Development
    • Pendleton, E., Bessette, D., Field, P., Miller, G., and Griffin, K., "Active Aeroelastic Wing Flight Research Program: Technical Program and Model Analytical Development," Journal of Aircraft, Vol. 37, No. 4, 2000, pp. 554-561.
    • (2000) Journal of Aircraft , vol.37 , Issue.4 , pp. 554-561
    • Pendleton, E.1    Bessette, D.2    Field, P.3    Miller, G.4    Griffin, K.5
  • 11
    • 0029219120 scopus 로고    scopus 로고
    • Perry, B. and Cole, S. R., Summary of an Active Flexible Wing Program, Journal of Aircraft, 32, No. 1, 1995, pp. 10-15, also AIAA Paper 92-2080, April. 1992.
    • Perry, B. and Cole, S. R., "Summary of an Active Flexible Wing Program," Journal of Aircraft, Vol. 32, No. 1, 1995, pp. 10-15, also AIAA Paper 92-2080, April. 1992.
  • 12
    • 0029223739 scopus 로고
    • Rolling Maneuver Load Alleviation Using ACtive Control
    • Woods-Vedler, J.A. Pototzky, A. and Hoadley, S., "Rolling Maneuver Load Alleviation Using ACtive Control," Journal of Aircraft, Vol. 32, No. 1, 1995, pp. 68-76.
    • (1995) Journal of Aircraft , vol.32 , Issue.1 , pp. 68-76
    • Woods-Vedler, J.A.1    Pototzky, A.2    Hoadley, S.3
  • 13
    • 34547493945 scopus 로고    scopus 로고
    • H.Rae, W. and Pope, A., Low speed Wind Tunnel Testing, John Wiley and Sons, New York, 1984.
    • H.Rae, W. and Pope, A., Low speed Wind Tunnel Testing, John Wiley and Sons, New York, 1984.
  • 16
    • 34247097252 scopus 로고    scopus 로고
    • Active Control of a Three Surface Wind Tunnel Aeroelastic Demonstrator: Modelling and Correlations
    • Munich, June 28, July 1
    • Scotti, A., Ricci, S., and Quaranta, G., "Active Control of a Three Surface Wind Tunnel Aeroelastic Demonstrator: Modelling and Correlations," Proceedings of the IFASD International Forum on Aeroelasticity, Munich, June 28 - July 1 2005.
    • (2005) Proceedings of the IFASD International Forum on Aeroelasticity
    • Scotti, A.1    Ricci, S.2    Quaranta, G.3
  • 18
    • 28844476045 scopus 로고    scopus 로고
    • Design of a control system for a canard foreplane applied to a three surface model for aeroelastic wind tunnel testing,
    • Feb, M.Eng. Thesis
    • Zanotti, D., "Design of a control system for a canard foreplane applied to a three surface model for aeroelastic wind tunnel testing," Feb 2003, M.Eng. Thesis.
    • (2003)
    • Zanotti, D.1
  • 19
    • 34547534146 scopus 로고    scopus 로고
    • Progetto e validazione di un modello di ala a freccia negativa con contrallo attivo multi-superficie,
    • M.Eng. Thesis
    • De Gaspari, A. and Riccobene, L., "Progetto e validazione di un modello di ala a freccia negativa con contrallo attivo multi-superficie," 2006, M.Eng. Thesis.
    • (2006)
    • De Gaspari, A.1    Riccobene, L.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.