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Volumn , Issue , 2010, Pages

Experimental determination of unsteady aerodynamic coefficients and flutter behavior of a rigid wing

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC MODELS; AEROELASTIC BEHAVIOR; AEROELASTIC MODELS; AIR SPEED; CRITICAL VALUE; DISCRETE-TIME; DYNAMIC PRESSURES; EXPERIMENTAL DETERMINATION; EXPERIMENTAL METHODS; EXPERIMENTAL PROCEDURE; FLUTTER SPEED; GROUND VIBRATION TESTS; LOW SPEED; MOTION SENSORS; PRESSURE DATA; REDUCED ORDER; STATE-SPACE; STRUCTURAL MODELS; SUB-CRITICAL; SUBSONIC WIND TUNNELS; SYSTEM IDENTIFICATION METHODS; TIME HISTORY; UNSTEADY AERODYNAMIC FORCE; UNSTEADY AERODYNAMICS; VARIABLE DYNAMICS;

EID: 84855635322     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (1)

References (9)
  • 1
    • 0242273110 scopus 로고    scopus 로고
    • Flight-test evaluation of flutter prediction methods
    • September-October
    • Lind, R., "Flight-Test Evaluation of Flutter Prediction Methods", Journal of Aircraft, Vol. 40, No. 5, September-October 2003, pp. 964-970.
    • (2003) Journal of Aircraft , vol.40 , Issue.5 , pp. 964-970
    • Lind, R.1
  • 2
    • 0035270437 scopus 로고    scopus 로고
    • Flutter prediction from flight flutter test data
    • March-April
    • Dimitriadis, G. and Cooper, J.E., "Flutter Prediction from Flight Flutter Test Data", Journal of Aircraft, Vol. 38, No. 2, March-April 2001, pp. 355-367.
    • (2001) Journal of Aircraft , vol.38 , Issue.2 , pp. 355-367
    • Dimitriadis, G.1    Cooper, J.E.2
  • 4
    • 0027660898 scopus 로고
    • Envelope function- A tool for analyzing flutter data
    • September-October
    • Cooper, J.E., Emmett, P.R., and Wright, J.R., "Envelope Function-A Tool for Analyzing Flutter Data", Journal of Aircraft, Vol. 30, No. 5, September-October 1993, pp. 785-790.
    • (1993) Journal of Aircraft , vol.30 , Issue.5 , pp. 785-790
    • Cooper, J.E.1    Emmett, P.R.2    Wright, J.R.3
  • 5
    • 85007688839 scopus 로고
    • Prediction of flutter onset speed based on flight testing at subcritical speeds
    • July-August
    • Zimmerman, N.H., Weissenburger, J.T., "Prediction of Flutter Onset Speed Based on Flight Testing at Subcritical Speeds," Journal of Aircraft, Vol. 1, No. 4, July-August 1964, pp. 190-202.
    • (1964) Journal of Aircraft , vol.1 , Issue.4 , pp. 190-202
    • Zimmerman, N.H.1    Weissenburger, J.T.2
  • 6
    • 0035082795 scopus 로고    scopus 로고
    • Flutter margin evaluation for discrete-time systems
    • January-February
    • Torii, H., and Matsuzaki, Y., "Flutter Margin Evaluation for Discrete-Time Systems", Journal of Aircraft, Vol. 38, No. 1, January-February 2001, pp. 42-47.
    • (2001) Journal of Aircraft , vol.38 , Issue.1 , pp. 42-47
    • Torii, H.1    Matsuzaki, Y.2
  • 7
    • 0024686307 scopus 로고
    • Method for experimental determination of flutter speed by parameter identification
    • Nissim, E., and Gilyard, G.B., "Method for Experimental Determination of Flutter Speed by Parameter Identification", NASA Technical Paper 2923, 1989.
    • (1989) NASA Technical Paper 2923
    • Nissim, E.1    Gilyard, G.B.2
  • 8
    • 80053445119 scopus 로고    scopus 로고
    • New system identification for couple fluid-structure systems: Aerodynamics is aeroelasticity minus structure
    • Seattle, WA, June
    • Kim, T., "New System Identification for Couple Fluid-Structure Systems: Aerodynamics is Aeroelasticity Minus Structure," IFASD-2009-073, International Forum on Aeroelasticity and Structural Dynamics, Seattle, WA, June, 2009.
    • (2009) IFASD-2009-073, International Forum on Aeroelasticity and Structural Dynamics
    • Kim, T.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.