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Volumn 9, Issue , 2005, Pages 6141-6150

Supersonic flutter and LCO of airfoils via CFD/analytical combined approach

Author keywords

[No Author keywords available]

Indexed keywords

EULER CODES; SUPERSONIC FLIGHT REGIMES;

EID: 28844455673     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper
Times cited : (4)

References (17)
  • 1
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    • Aeroelastic response of a 2-D lifting surfaces to gust and arbitrary explosive loading signatures
    • Marzocca, P., Librescu, L., and Chiocchia, G., "Aeroelastic Response of a 2-D Lifting Surfaces to Gust and Arbitrary Explosive Loading Signatures," International Journal of Impact Engineering, Vol. 25, No. 1, 2001, pp. 41-65.
    • (2001) International Journal of Impact Engineering , vol.25 , Issue.1 , pp. 41-65
    • Marzocca, P.1    Librescu, L.2    Chiocchia, G.3
  • 2
    • 0036086175 scopus 로고    scopus 로고
    • Aeroelastic response of a 2-D airfoil in compressible flight speed regimes exposed to blast loadings
    • Marzocca, P., Librescu, L., and Chiocchia, G., "Aeroelastic Response of a 2-D Airfoil in Compressible Flight Speed Regimes Exposed to Blast Loadings," Aerospace Science and Technology, Vol. 6, No. 4, 2002, pp. 259-272.
    • (2002) Aerospace Science and Technology , vol.6 , Issue.4 , pp. 259-272
    • Marzocca, P.1    Librescu, L.2    Chiocchia, G.3
  • 3
    • 85087192296 scopus 로고    scopus 로고
    • Aeroelastic response of swept aircraft wings in a compressible flow field
    • AIAA Paper 2001-0714, January 8-11 Reno, NV
    • Marzocca, P., Librescu, L., and Silva, W. A., "Aeroelastic Response of Swept Aircraft Wings in a Compressible Flow Field," AIAA Paper 2001-0714, 39th AIAA Aerospace Sciences Meeting, January 8-11, 2001, Reno, NV.
    • (2001) 39th AIAA Aerospace Sciences Meeting
    • Marzocca, P.1    Librescu, L.2    Silva, W.A.3
  • 5
    • 17444383268 scopus 로고    scopus 로고
    • Development of a nonlinear indicial model for maneuvering fighter aircraft
    • AIAA Paper 96-0896, Reno, Nevada, January
    • Reisenthel, P. H., "Development of a Nonlinear Indicial Model for Maneuvering Fighter Aircraft," AIAA Paper 96-0896, 34th Aerospace Sciences Meeting, Reno, Nevada, January 1996.
    • (1996) 34th Aerospace Sciences Meeting
    • Reisenthel, P.H.1
  • 8
    • 0018452920 scopus 로고
    • Unsteady aerodynamic modeling for arbitrary motions
    • Edwards, J. W., Ashley, H., and Breakwell, J.V., "Unsteady Aerodynamic Modeling for Arbitrary Motions," AIAA Journal, Vol. 17, No. 4, 1979, pp. 365-374.
    • (1979) AIAA Journal , vol.17 , Issue.4 , pp. 365-374
    • Edwards, J.W.1    Ashley, H.2    Breakwell, J.V.3
  • 10
    • 0003949807 scopus 로고    scopus 로고
    • Cambridge, New York, Cambridge University Press, Cambridge aerospace series, 12
    • Leishman, J. G., Principles of Helicopter Aerodynamics, Cambridge, New York, Cambridge University Press, 2000, Cambridge aerospace series, 12.
    • (2000) Principles of Helicopter Aerodynamics
    • Leishman, J.G.1
  • 11
    • 0038839484 scopus 로고
    • Identification of aerodynamic indicial functions using flight data
    • AIAA Paper 82-1375, 9th, San Diego, CA, August
    • Gupta, N. K., and Iliff, K. W., "Identification of Aerodynamic Indicial Functions Using Flight Data," AIAA Paper 82-1375, AIAA Atmospheric Flight Mechanics Conference, 9th, San Diego, CA, August 1982.
    • (1982) AIAA Atmospheric Flight Mechanics Conference
    • Gupta, N.K.1    Iliff, K.W.2
  • 12
    • 0034224009 scopus 로고    scopus 로고
    • Transonic and low-supersonic aeroelastic analysis of two degree of freedom airfoil with freeplay non-linearity
    • Kim, D. H. and Lee, I., "Transonic and Low-Supersonic Aeroelastic Analysis of Two Degree of Freedom Airfoil with Freeplay Non-linearity," Journal of Sound and Vibration, Vol. 234, No. 5, 2000, pp. 859-880.
    • (2000) Journal of Sound and Vibration , vol.234 , Issue.5 , pp. 859-880
    • Kim, D.H.1    Lee, I.2
  • 15
    • 0009162870 scopus 로고
    • Numerical determination of indicial lift of a two-dimensional sinking airfoil at subsonic mach numbers from oscillatory lift coefficients with calculations for mach number 0.7
    • Mazelsky, B., "Numerical Determination of Indicial Lift of a Two-dimensional Sinking Airfoil at Subsonic Mach Numbers from Oscillatory Lift Coefficients with Calculations for Mach Number 0.7," NACA TN 2562, 1951
    • (1951) NACA TN , vol.2562
    • Mazelsky, B.1
  • 16
    • 84888885959 scopus 로고
    • and NACA TN 2613, 1952.
    • (1952) NACA TN , vol.2613
  • 17
    • 0009232539 scopus 로고
    • The indicial lift and pitching moment for a sinking or pitching two-dimensional wing flying at subsonic or supersonic speeds
    • Lomax, H., Heaslet, M. A., and Sluder, L., "The Indicial Lift and Pitching Moment for a Sinking or Pitching Two-Dimensional Wing Flying at Subsonic or Supersonic Speeds," NACA TN 2403, 1951.
    • (1951) NACA TN , vol.2403
    • Lomax, H.1    Heaslet, M.A.2    Sluder, L.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.