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Volumn 22, Issue 1, 1999, Pages 168-171

Flutter boundary prediction using physical models and experimental data

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT DYNAMICS; FLUTTER (AERODYNAMICS); MATHEMATICAL MODELS; WIND TUNNELS;

EID: 0032762283     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.7621     Document Type: Article
Times cited : (13)

References (12)
  • 3
    • 0142161626 scopus 로고    scopus 로고
    • Ph.D. Thesis, Dept. of Aeronautics and Astronautics, Massachusetts Inst. of Technology, Cambridge, MA, Feb.
    • Lin, C., "Towards Optimal Strain Actuated Aeroelastic Control," Ph.D. Thesis, Dept. of Aeronautics and Astronautics, Massachusetts Inst. of Technology, Cambridge, MA, Feb. 1996.
    • (1996) Towards Optimal Strain Actuated Aeroelastic Control
    • Lin, C.1
  • 5
    • 0015160179 scopus 로고
    • An Approximate True Damping Solution of the Flutter Equation by Determinant Iteration
    • Hassig, H., "An Approximate True Damping Solution of the Flutter Equation by Determinant Iteration," Journal of Aircraft, Vol. 8, No. 11, 1971, pp. 885-889.
    • (1971) Journal of Aircraft , vol.8 , Issue.11 , pp. 885-889
    • Hassig, H.1
  • 6
    • 84889232241 scopus 로고
    • Method for Experimental Determination of Flutter Speed by Parameter Identification
    • AIAA, Washington, DC, April (AIAA Paper 89-1324, 1989)
    • Nissim, E., and Gilyard, G. B., "Method for Experimental Determination of Flutter Speed by Parameter Identification," 30th Structures, Structural Dynamics, and Materials Conference, AIAA, Washington, DC, April 1989, pp. 1427-1441 (AIAA Paper 89-1324, 1989).
    • (1989) 30th Structures, Structural Dynamics, and Materials Conference , pp. 1427-1441
    • Nissim, E.1    Gilyard, G.B.2
  • 7
    • 0031139413 scopus 로고    scopus 로고
    • Robust Flutter Margins of an F/A-18 Aircraft from Aeroelastic Flight Data
    • Brenner, M., and Lind, R., "Robust Flutter Margins of an F/A-18 Aircraft from Aeroelastic Flight Data," Journal of Guidance, Control, and Dynamics, Vol. 20, No. 3,1997, pp. 597-604.
    • (1997) Journal of Guidance, Control, and Dynamics , vol.20 , Issue.3 , pp. 597-604
    • Brenner, M.1    Lind, R.2
  • 8
    • 0032075159 scopus 로고    scopus 로고
    • Time-Frequency Analysis for the Transfer Function Estimation and Application to Flutter Clearance
    • Feron, E., Brenner, M., Paduano, J., and Turevskiy, A., "Time-Frequency Analysis for the Transfer Function Estimation and Application to Flutter Clearance," Journal of Guidance, Control, and Dynamics, Vol. 21, No. 3, 1998, pp. 375-382.
    • (1998) Journal of Guidance, Control, and Dynamics , vol.21 , Issue.3 , pp. 375-382
    • Feron, E.1    Brenner, M.2    Paduano, J.3    Turevskiy, A.4
  • 9
    • 0030289780 scopus 로고    scopus 로고
    • Minimum-State Unsteady Aerodynamic Approximations with Flexible Constraints
    • Karpel, M., and Strul, E., "Minimum-State Unsteady Aerodynamic Approximations with Flexible Constraints," Journal of Aircraft, Vol. 33, No. 6, 1996, pp. 1190-1196.
    • (1996) Journal of Aircraft , vol.33 , Issue.6 , pp. 1190-1196
    • Karpel, M.1    Strul, E.2
  • 12
    • 0029224976 scopus 로고
    • An Active Aeroelastic Wing Model for Vibration and Flutter Suppression
    • AIAA, Washington, DC, April (AIAA Paper 95-1193, 1995)
    • Reich, G., VanSchoor, M., Lin, C., and Crawley, E., "An Active Aeroelastic Wing Model for Vibration and Flutter Suppression," 36th Structures, Structural Dynamics, and Materials Conference, AIAA, Washington, DC, April 1995, pp. 314-324 (AIAA Paper 95-1193, 1995).
    • (1995) 36th Structures, Structural Dynamics, and Materials Conference , pp. 314-324
    • Reich, G.1    VanSchoor, M.2    Lin, C.3    Crawley, E.4


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.