메뉴 건너뛰기




Volumn 20, Issue 5, 2006, Pages 1044-1066

Control of an all-movable foreplane for a three surfaces aircraft wind tunnel model

Author keywords

Aeroelastic model; Real time control; Vibration control

Indexed keywords

AERODYNAMICS; COMPUTER SIMULATION; COMPUTER SOFTWARE; REAL TIME SYSTEMS; VIBRATION CONTROL; WIND TUNNELS;

EID: 33644610020     PISSN: 08883270     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ymssp.2005.08.020     Document Type: Article
Times cited : (13)

References (18)
  • 2
    • 0006340092 scopus 로고
    • Reduction of structural loads using maneuver load control on the advanced Fighter technology integration (AFTI) mission adaptive wing
    • NASA
    • S.V. Thornton, Reduction of structural loads using maneuver load control on the advanced Fighter technology integration (AFTI) mission adaptive wing, Technical Report TM-4526, NASA, 1993.
    • (1993) Technical Report , vol.TM-4526
    • Thornton, S.V.1
  • 3
    • 0034226416 scopus 로고    scopus 로고
    • The active aeroelastic wing flight research program: Technical program and model analytical development
    • E. Pendleton, D. Bessette, P. Field, G. Miller, and K. Griffin The active aeroelastic wing flight research program: technical program and model analytical development J. Aircraft 37 4 2000 554 561
    • (2000) J. Aircraft , vol.37 , Issue.4 , pp. 554-561
    • Pendleton, E.1    Bessette, D.2    Field, P.3    Miller, G.4    Griffin, K.5
  • 4
    • 0035472772 scopus 로고    scopus 로고
    • Adaptive wing and ow control technology
    • E. Stanewsky Adaptive wing and ow control technology Progress in Aerospace Sciences 37 2001 583 667
    • (2001) Progress in Aerospace Sciences , vol.37 , pp. 583-667
    • Stanewsky, E.1
  • 6
    • 0035516874 scopus 로고    scopus 로고
    • Maneuver trim optimization techniques for active aeroelastic wings
    • P.S. Zink, D.N. Mavris, and D.E. Raveh Maneuver trim optimization techniques for active aeroelastic wings J. Aircraft 38 6 2001 1139 1146
    • (2001) J. Aircraft , vol.38 , Issue.6 , pp. 1139-1146
    • Zink, P.S.1    Mavris, D.N.2    Raveh, D.E.3
  • 9
    • 0007322372 scopus 로고
    • Flutter suppression using active controls based on the concept of aerodynamic energy
    • National Aeronautics and Space Administration
    • E. Nissim, Flutter suppression using active controls based on the concept of aerodynamic energy, National Aeronautics and Space Administration, NASA TN-6199, 1971.
    • (1971) NASA TN-6199
    • Nissim, E.1
  • 10
    • 0042598007 scopus 로고
    • Design, test and evaluation of three active flutter suppression controllers
    • National Aeronautics and Space Administration
    • W.M. Adams, D.M. Christhilf, Jr., M.R. Waszak, V. Mukhopadhyay, S. Srinathkumar, Design, test and evaluation of three active flutter suppression controllers, National Aeronautics and Space Administration, NASA TM-4338, 1992.
    • (1992) NASA TM-4338
    • Adams, W.M.1    Christhilf Jr., D.M.2    Waszak, M.R.3    Mukhopadhyay, V.4    Srinathkumar, S.5
  • 12
    • 0141913335 scopus 로고
    • Flight investigation of a structural mode control system for XB-70 Aircraft
    • National Aeronautics and Space Administration
    • W.P. Lock, E. Kordes, J.M. McKay, J.H. Wykes, Flight investigation of a structural mode control system for XB-70 Aircraft, National Aeronautics and Space Administration, NASA TN D-7420, 1973.
    • (1973) NASA TN , vol.D-7420
    • Lock, W.P.1    Kordes, E.2    McKay, J.M.3    Wykes, J.H.4
  • 15
    • 0032649041 scopus 로고    scopus 로고
    • Single finite states modeling of aerodynamic forces related to structural motion and gusts
    • G. Pasinetti, and P. Mantegazza Single finite states modeling of aerodynamic forces related to structural motion and gusts AIAA JOURNAL 37 5 1999 604 612
    • (1999) AIAA JOURNAL , vol.37 , Issue.5 , pp. 604-612
    • Pasinetti, G.1    Mantegazza, P.2
  • 17
    • 27744567158 scopus 로고
    • In-flight lift-drag Characteristics for a forward-swept wing aircraft (and Comparisons with Contemporary Aircraft): National Aeronautics and Space Administration
    • E.J. Saltzman, J.J. Hicks, In-flight lift-drag Characteristics for a forward-swept wing aircraft (and Comparisons With Contemporary Aircraft): National Aeronautics and Space Administration, NASA Technical Paper 3414, 1994.
    • (1994) NASA Technical Paper , vol.3414
    • Saltzman, E.J.1    Hicks, J.J.2
  • 18
    • 1042305068 scopus 로고
    • Design and experimental validation of a flutter suppression controller for the active flexible wing
    • National Aeronautics and Space Administration
    • M.R. Waszak, S. Srimathkumar, Design and experimental validation of a flutter suppression controller for the active flexible wing, National Aeronautics and Space Administration, NASA TM-4381, 1992.
    • (1992) NASA TM-4381
    • Waszak, M.R.1    Srimathkumar, S.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.