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Volumn , Issue , 2004, Pages 4503-4516

Aero-structural wing planform optimization

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; DRAG; FUSELAGES; MATHEMATICAL MODELS; OPTIMIZATION; PARTIAL DIFFERENTIAL EQUATIONS; PROBLEM SOLVING; VECTORS;

EID: 2942714974     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2004-29     Document Type: Conference Paper
Times cited : (13)

References (16)
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    • Computational aerodynamics for aircraft design
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    • Jameson, A.1
  • 4
    • 0035245857 scopus 로고    scopus 로고
    • A perspective on computational algorithms for aerodynamic analysis and design
    • A. Jameson. A perspective on computational algorithms for aerodynamic analysis and design. Progress in Aerospace Sciences, 37:197-243, 2001.
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    • Jameson, A.1
  • 5
    • 0347038536 scopus 로고    scopus 로고
    • Aerodynamic shape optimization techniques based on control theory
    • CIME (International Mathematical Summer Center), Martina Franca, Italy
    • A. Jameson and L. Martinelli. Aerodynamic shape optimization techniques based on control theory. Technical report, CIME (International Mathematical Summer Center), Martina Franca, Italy, 1999.
    • (1999) Technical Report
    • Jameson, A.1    Martinelli, L.2
  • 6
    • 85085404450 scopus 로고    scopus 로고
    • Computational fluid dynamics for aerodynamic design: Its current and future impact
    • AIAA Paper 2001-0538, Reno, NV, January
    • J. C. Vassberg and A. Jameson. Computational fluid dynamics for aerodynamic design: Its current and future impact. AIAA paper 2001-0538, AIAA 39th Aerospace Sciences Meeting & Exhibit, Reno, NV, January 2001.
    • (2001) AIAA 39th Aerospace Sciences Meeting & Exhibit
    • Vassberg, J.C.1    Jameson, A.2
  • 8
    • 85085776119 scopus 로고    scopus 로고
    • Design optimization of high-lift configurations using a viscous continuous adjoint method
    • AIAA Paper 2002-0844, Reno, NV, January
    • S. Kim, J. J. Alonso, and A. Jameson. Design optimization of high-lift configurations using a viscous continuous adjoint method. AIAA paper 2002-0844, AIAA 40th Aerospace Sciences Meeting & Exhibit, Reno, NV, January 2002.
    • (2002) AIAA 40th Aerospace Sciences Meeting & Exhibit
    • Kim, S.1    Alonso, J.J.2    Jameson, A.3
  • 9
    • 85086492356 scopus 로고    scopus 로고
    • Aerodynamic shape optimization of wings including planform variables
    • AIAA Paper 2002-0210, Reno, Nevada, January
    • K. Leoviriyakit and A. Jameson. Aerodynamic shape optimization of wings including planform variables. AIAA paper 2002-0210, 41st Aerospace Sciences Meeting & Exhibit, Reno, Nevada, January 2003.
    • (2003) 41st Aerospace Sciences Meeting & Exhibit
    • Leoviriyakit, K.1    Jameson, A.2
  • 10
    • 2942750760 scopus 로고
    • Lifting surface design using multidisplinary optimization
    • Stanford University Doctoral Dissertation, Stanford, CA
    • S. Wakayama. Lifting surface design using multidisplinary optimization. Technical report, Stanford University Doctoral Dissertation, Stanford, CA, 1994.
    • (1994) Technical Report
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  • 11
    • 2942756966 scopus 로고
    • Design and analysis of optimally-loaded lifting systems
    • October
    • I. M. Kroo. Design and analysis of optimally-loaded lifting systems. AIAA paper 1984-2507, October 1984.
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  • 12
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    • An automated method for sensitivity analysis using complex variables
    • AIAA Paper 2000-0689, Reno, Nevada, January
    • J. R. R. A. Martins, I. M. Kroo, and J. J. Alonso. An automated method for sensitivity analysis using complex variables. AIAA paper 2000-0689, 38th Aerospace Sciences Meeting, Reno, Nevada, January 2000.
    • (2000) 38th Aerospace Sciences Meeting
    • Martins, J.R.R.A.1    Kroo, I.M.2    Alonso, J.J.3
  • 13
    • 2942712384 scopus 로고
    • Generating derivative codes from Fortran programs
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    • (1991) Internal Report , vol.MCS-P263-0991
    • Bischof, C.1    Carle, A.2    Corliss, G.3    Griewank, A.4    Hovland, P.5
  • 14
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    • Analysis and design of numerical schemes for gas dynamics 1, artificial diffusion, upwind biasing, limiters and their effect on multigrid convergence
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    • (1995) Int. J. of Comp. Fluid Dyn. , vol.4 , pp. 171-218
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  • 15
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    • Analysis and design of numerical schemes for gas dynamics 2, artificial diffusion and discrete shock structure
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  • 16
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    • A gradient accuracy study for the adjoint-based Navier-Stokes design method
    • AIAA Paper 1999-0299, Reno, Nevada, January
    • S. Kim, J. J. Alonso, and A. Jameson. A gradient accuracy study for the adjoint-based Navier-Stokes design method. AIAA paper 1999-0299, 37th Aerospace Science Meething & Exhibit, Reno, Nevada, January 1999.
    • (1999) 37th Aerospace Science Meething & Exhibit
    • Kim, S.1    Alonso, J.J.2    Jameson, A.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.