메뉴 건너뛰기




Volumn , Issue , 2000, Pages

Aircraft aeroelastic analysis and design using CFD-based unsteady loads

Author keywords

[No Author keywords available]

Indexed keywords

FLUTTER (AERODYNAMICS); MACH NUMBER; STEP RESPONSE; STRUCTURAL ANALYSIS; STRUCTURAL DYNAMICS; SUPERSONIC AIRCRAFT; TRANSONIC FLOW; WIND TUNNELS;

EID: 85088760690     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-1325     Document Type: Conference Paper
Times cited : (25)

References (26)
  • 1
    • 0020799497 scopus 로고
    • Transonic Time-Response Analysis of 3-Degree-of-Freedom Conventional and Supercritical Airfoils
    • August
    • Yang H. T. Y. and Batina J. T. Transonic Time-Response Analysis of 3-Degree-of-Freedom Conventional and Supercritical Airfoils. Journal of Aircraft, 20(8):703-710, August 1983.
    • (1983) Journal of Aircraft , vol.20 , Issue.8 , pp. 703-710
    • Yang, H.T.Y.1    Batina, J.T.2
  • 2
    • 0024091975 scopus 로고
    • Modern Wing Flutter Analysis by Computational Fluid Dynamics Method
    • October Dynamics Method. Journal of Aircraft, 25(10):962-968, October 1988
    • Cunningham H. J., Batina J. T., and Bennett R. M. Modern Wing Flutter Analysis by Computational Fluid Dynamics Method. Journal of Aircraft, 25(10):962-968, October 1988. Dynamics Method. Journal of Aircraft, 25(10):962-968, October 1988.
    • (1988) Journal of Aircraft , vol.25 , Issue.10 , pp. 962-968
    • Cunningham, H.J.1    Batina, J.T.2    Bennett, R.M.3
  • 3
    • 0025434028 scopus 로고
    • Euler Flutter Analysis of Airfoils Using Unstructured Dynamic Meshes
    • May
    • Rausch R. D., Batina J. T., and Yang H. T. Y. Euler Flutter Analysis of Airfoils Using Unstructured Dynamic Meshes. Journal of Aircraft, 27(5):436-443, May 1990.
    • (1990) Journal of Aircraft , vol.27 , Issue.5 , pp. 436-443
    • Rausch, R.D.1    Batina, J.T.2    Yang, H.T.Y.3
  • 4
    • 0026261105 scopus 로고
    • Aeroelastic Analysis of Wings Using the Euler Equations with Deforming Mesh
    • November
    • Robinson B. A., Batina J. T., and Yang H. T. Y. Aeroelastic Analysis of Wings Using the Euler Equations with Deforming Mesh. Journal of Aircraft, 28(11):781-788, November 1991.
    • (1991) Journal of Aircraft , vol.28 , Issue.11 , pp. 781-788
    • Robinson, B.A.1    Batina, J.T.2    Yang, H.T.Y.3
  • 5
    • 0029277237 scopus 로고
    • Wing Flutter Boundary Prediction Using Unsteady Euler Aerodynamic Method
    • March
    • Lee-Rausch E. M. and Batina J. T. Wing Flutter Boundary Prediction Using Unsteady Euler Aerodynamic Method. Journal of Aircraft, 32(2):416-422, March 1995.
    • (1995) Journal of Aircraft , vol.32 , Issue.2 , pp. 416-422
    • Lee-Rausch, E.M.1    Batina, J.T.2
  • 6
    • 0030289123 scopus 로고    scopus 로고
    • Wing Flutter Computations Using an Aerodynamic Model Based on the Navier-Stokes Equations
    • November
    • Lee-Rausch E. M. and Batina J. T. Wing Flutter Computations Using an Aerodynamic Model Based on the Navier-Stokes Equations. Journal of Aircraft, 33(6): 1139-1147, November 1996.
    • (1996) Journal of Aircraft , vol.33 , Issue.6 , pp. 1139-1147
    • Lee-Rausch, E.M.1    Batina, J.T.2
  • 7
    • 0024770422 scopus 로고
    • Mach Number Effects on Transonic Aeroelastic Forces and Flutter Characteristics
    • November
    • Mohr R. W., Batina J. T., and Yang H. T. Y. Mach Number Effects on Transonic Aeroelastic Forces and Flutter Characteristics. Journal of Aircraft, 26(11): 1038-1046, November 1989.
    • (1989) Journal of Aircraft , vol.26 , Issue.11 , pp. 1038-1046
    • Mohr, R.W.1    Batina, J.T.2    Yang, H.T.Y.3
  • 9
    • 0001134482 scopus 로고    scopus 로고
    • Reduced-order models based on linear and nonlinear aerodynamic impulse response
    • In Williamsburg, VA, June
    • Silva W. A. Reduced-order models based on linear and nonlinear aerodynamic impulse response. In International Forum on Aeroelasticity and Structural Dynamics, pages 369-379, Williamsburg, VA, June 1999.
    • (1999) International Forum on Aeroelasticity and Structural Dynamics , pp. 369-379
    • Silva, W.A.1
  • 11
    • 84983121978 scopus 로고    scopus 로고
    • Development of discrete-time aerodynamic model for cfd-based aeroelastic analysis
    • In Reno, NV, January. AIAA-99-0765
    • Cowan T. J., Arena A. S. Jr., and Gupta K. K. Development of discrete-time aerodynamic model for cfd-based aeroelastic analysis. In 37th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 1999. AIAA-99-0765.
    • (1999) 37th AIAA Aerospace Sciences Meeting and Exhibit
    • Cowan, T.J.1    Arena Jr., A.S.2    Gupta, K.K.3
  • 12
    • 0027664172 scopus 로고
    • Application of Nonlinear Systems Theory to Transonic Unsteady Aerodynamic Responses
    • September
    • Silva W. A. Application of Nonlinear Systems Theory to Transonic Unsteady Aerodynamic Responses. Journal of Aircraft, 30(5):660-668, September 1993.
    • (1993) Journal of Aircraft , vol.30 , Issue.5 , pp. 660-668
    • Silva, W.A.1
  • 13
    • 0027274399 scopus 로고
    • Extension of a Nonlinear System Theory to General-Frequency Unsteady Transonic Aerodynamic Responses
    • In La Jolla, CA, April. AIAA-93-1590
    • Silva W. A. Extension of a Nonlinear System Theory to General-Frequency Unsteady Transonic Aerodynamic Responses. In 34th Structures, Structural Dynamics, and Materials Conference, La Jolla, CA, April 1993. AIAA-93-1590.
    • (1993) 34th Structures, Structural Dynamics, and Materials Conference
    • Silva, W.A.1
  • 14
    • 84983110887 scopus 로고    scopus 로고
    • Identification of Linear and Nonlinear Aerodynamic Impulse Response Using Digital Filter Techniques
    • In New Orleans, LA, August. AIAA-97-3712
    • Silva W. A. Identification of Linear and Nonlinear Aerodynamic Impulse Response Using Digital Filter Techniques. In AIAA Atmospheric Flight Mechanics Conference, New Orleans, LA, August 1997. AIAA-97-3712.
    • (1997) AIAA Atmospheric Flight Mechanics Conference
    • Silva, W.A.1
  • 16
    • 0017932980 scopus 로고
    • Computation of unsteady transonic flows by indicial methods
    • February
    • Ballhaus W. F. and Goorjian P. M. Computation of unsteady transonic flows by indicial methods. AIAA Journal, 16(2):117-124, February 1978.
    • (1978) AIAA Journal , vol.16 , Issue.2 , pp. 117-124
    • Ballhaus, W.F.1    Goorjian, P.M.2
  • 20
    • 0033326510 scopus 로고    scopus 로고
    • Structural optimization of flight vehicles with computational-fluid-dynamics-based maneuver loads
    • November-December
    • Raveh. D. E. and Karpel. M. Structural optimization of flight vehicles with computational-fluid-dynamics-based maneuver loads. Journal of Aircraft, 36(6):1007-1015, November-December 1999.
    • (1999) Journal of Aircraft , vol.36 , Issue.6 , pp. 1007-1015
    • Raveh, D.E.1    Karpel, M.2
  • 23
    • 0004826924 scopus 로고    scopus 로고
    • Zona Technologies, Scottsdale, AZ. 99-24.4 edition, November
    • Zona Technologies, Scottsdale, AZ. ZAERO Theoretical Manual, 99-24.4 edition, November 1999.
    • (1999) ZAERO Theoretical Manual
  • 25
    • 0004894492 scopus 로고    scopus 로고
    • Zona Technologies, Scottsdale, AZ. 99-24.3 edition, November
    • Zona Technologies, Scottsdale, AZ. ZAERO Applications Manual, 99-24.3 edition, November 1999.
    • (1999) ZAERO Applications Manual
  • 26
    • 0032074002 scopus 로고    scopus 로고
    • Modal based enhancement of integrated design optimization schemes
    • May
    • Modal based enhancement of integrated design optimization schemes. Journal of Aircraft, 35(3):437-444, May 1998.
    • (1998) Journal of Aircraft , vol.35 , Issue.3 , pp. 437-444


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.