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All issues Volume 6 / No 3 (2011) Math. Model. Nat. Phenom., 6 3 (2011) 166-188 References
Free Access
Issue
Math. Model. Nat. Phenom.
Volume 6, Number 3, 2011
Computational aerodynamics
Page(s) 166 - 188
DOI https://doi.org/10.1051/mmnp/20116307
Published online 16 May 2011
  1. J. J. Alonso, J.R. Martins, J. J. Reuther, R. Haimes, C. A. Crawford. High-fidelity aero-structural design using a parametric CAD-based model.16th AIAA Computational Fluid Dynamics Conference, Orlando, FL, June 23- 26, 2003, AIAA-2003-3429. [Google Scholar]
  2. K. J. Badcock, B. E. Richards, M. A. Woodgate. Elements of computational fluid dynamics on block structured grids using implicit solvers. Progress in Aerospace Sciences, 36 (2000), 351-392. [CrossRef] [Google Scholar]
  3. J. T. Baker. Mesh generation: Art or science? Progress in Aerospace Sciences, 41 (2005), 29-63. [CrossRef] [Google Scholar]
  4. K. Becker, J. Vassberg. Numerical aerodynamics in transport aircraft design. Notes on Num. Fluid Mechanics, 100 (2009), 209-220. [CrossRef] [Google Scholar]
  5. A. Berard, A. Rizzi, A. T. Isikveren. CADac: a new geometry construction tool for aerospace vehicle pre-design and conceptual design. 26th Applied Aerodynamics Conference, Honolulu, Hawaii, USA, August 18-21, 2008, AIAA-2008-6219. [Google Scholar]
  6. A. Bergmann, A. Hubner, T. Loeser. Experimental and numerical research on the aerodynamics of unsteady moving aircraft. Progress in Aerospace Sciences, 44 (2008), 121-137. [CrossRef] [Google Scholar]
  7. W. B. Blake. Prediction of Fighter Aircraft Dynamic Derivatives Using Digital Datcom. AlAA 3rd Applied Aerodynamics Conference, Colorado Springs, Colorado, October 14-16, 1985, AIAA-85-4070. [Google Scholar]
  8. K. Bowcutt. A perspective on the future of aerospace vehicle design. 12th AIAA International Space Planes and Hypersonic Systems and Technologies, Norfolk, Virginia, Dec. 15-19, 2003, AIAA 2003-6957. [Google Scholar]
  9. G. E. Cooper. Understanding and interpreting pilot opinions. Aeron Eng. Rev., 16 (1957), No. 3, 47-51. [Google Scholar]
  10. P. Eliasson. EDGE, a Navier-Stokes solver for unstructured grids, finite volumes for complex applications III: problems and perspectives. Hermes Penton Science, London, 2002. [Google Scholar]
  11. J.R. Gloudemans, P. C. Davis, P. A. Gelhausen. A rapid geometry modeler for conceptual aircraft. 34th Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan. 15-18, 1996, AIAA-1996-0052. [Google Scholar]
  12. T. Goetzendorf-Grabowski, J. B. Vos, S. Sanchi, P. Molitor, M. Tomac, A. Rizzi. Coupling adaptive-fidelity CFD with S&C analysis to predict flying qualities. 27th AIAA Applied Aerodynamics Conference, San Antonio, Texas, June 22-25, 2009, AIAA-2009-3630. [Google Scholar]
  13. M. Ghoreyshi, K. J. Badcock, M. A. Woodgate. Accelerating the numerical generation of aerodynamic models for flight simulation. Journal of Aircraft, 46 (2009), No. 3, 972-980. [CrossRef] [Google Scholar]
  14. R. Haimes. CAPRI: Computational analysis programming interface. CAPRI technical guide, Massachusetts Institute of Technology, 1998. [Google Scholar]
  15. A. T. Isikveren. Quasi-analytical modelling and optimisation techniques for transport aircraft design. PhD Thesis, Department of Aeronautics, Royal Institute of Technology, Stockholm, Sweden, 2002. [Google Scholar]
  16. R. von Kaenel, A. Rizzi, J. Oppelstrup, T. Goetzendorf-Grabowski, M. Ghoreyshi, L. Cavagna, A. Berard. CEASIOM: simulating stability & control with CFD/CSM in aircraft conceptual design, 26th International Congress of the Aeronautical Sciences, ICAS, 2008. [Google Scholar]
  17. F. Ladeinde. Truely automatic CFD mesh generation with support for reverse engineering. Aerospace Sciences Meeting and Exhibit, 37th, Reno, NV, Jan. 11-14, 1999, AIAA 99-0828. [Google Scholar]
  18. R. Lohner. Automatic unstructured grid generators. Journal of Finite Elements in Analysis and Design, 25 (1997), 111-134. [CrossRef] [Google Scholar]
  19. R. Lohner, J. Cebral. Generation of non-isotropic unstructured grids via directional enrichment. International Journal for Numerical Methods in Engineering, 49 (2000), 219-232. [CrossRef] [Google Scholar]
  20. W. H. Mason, D. L. Knill, A. A. Giunta, B. Grossman, L. T. Watson, R. T. Haftka. Getting the full benefits of CFD in conceptual design. 16th Applied Aerodynamics Conference, Albuquerque, NM, June 15-18, 1998, AIAA 98-2513. [Google Scholar]
  21. D. N. Mavris, D. A. DeLaurentis, D. S. Soban. Probabilistic assessment of handling qualities characteristics in preliminary aircraft design. 36th Aerospace Sciences Meeting and Exhibit, Reno, NV, Jan. 12-15, 1998, AIAA 98-0492. [Google Scholar]
  22. B. Mialon, S. Ben Khelil, A. Huebner, J.-C. Jouhaud, G. Roge, S. Hitzel, K. Badcock, P. Eliasson, A. Khabrov, M. Lahuta. European benchmark on numerical prediction of stability and control derivatives. 27th AIAA Applied Aerodynamics Conference, San Antonio, TX, June 22-25, 2009, AIAA-2009-4116. [Google Scholar]
  23. D. J. McCormick. An analysis of using CFD in conceptual aircraft design, M.S. Thesis, Dept. of Mechanical Engineering, Virginia Polytechnic Institute, Blacksburg, VA, 2002. [Google Scholar]
  24. T. Melin, A. T. Isikveren, A. Rizzi, C. Stamblewski, H. V. Anders. How industry concepts of concurrent engineering enhance aircraft design education. Journal of Aerospace Engineering, 221 (2007), 175-192. [Google Scholar]
  25. D. P. Raymer. Aircraft design: A conceptual approach. AIAA Education Series, Reston, VA, USA, 2006, [Google Scholar]
  26. V. Razgonyaev, W.H. Mason. An evaluation of aerodynamic prediction methods applied to the XB-70 for use in high speed aircraft stability and control system design. 33rd Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 1995, AIAA-95-0759. [Google Scholar]
  27. S. E. Rogers, M. J. Aftomis, S. A. Pandya, N. M. Chaderjian, E. T. Tejnil, J. U. Ahmad. Automated CFD parameter studies on distributed parallel computers. 16th AIAA Computational Fluid Dynamics Conference, Orlando, Florida, 2003, AIAA 2003-4229. [Google Scholar]
  28. D. L. Rodriguez, P. Sturdza. A rapid geometry engine for preliminary aircraft design. 44th Aerospace Science Meeting and Exhibit, Reno, NV, Jan. 9-12, 2006, AIAA-2006-929. [Google Scholar]
  29. J. Roskam. Airplane design. Roskam Aviation and Engineering Corporation, Kansas, USA, 1990. [Google Scholar]
  30. J. E. Williams, S. R. Vukelich. The USAF stability and control digital DATCOM. McDonnell Douglas Astona UTICS Company, St Louis Division, St Louis, Missouri, AFFDL-TR-79-3032, 1979. [Google Scholar]

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