eCFD
Flow simulation at your fingertips
eCFD

References

  1. Boelens, O.J.; Badcock, K.J.; Goertz, S.; Morton, S.A.; Fritz, W.; Karman, S.L. Jr.; Michal, T.; Lamar, J.E., “F-16XL Geometry and Computational Grids Used in Cranked-Arrow Wing Aerodynamics Project International,” In: AIAA “ Journal of Aircraft, Vol 46, No. 2, pp 369-376, March-April 2009.
  2. Boelens, O. J.; Badcock, K. J.; Elmilgui, A.; Abdol-Hamid, K. S.; Massey, S. J.,” Comparison of Measured and Block Structured Simulations for the F-16XL Aircraft,” In: AIAA “ Journal of Aircraft, Vol 46, No. 2, pp 377-384, March-April 2009.
  3. Boelens, O. J., “CFD Analysis of the Flow Around the X-31 Aircraft at High Angle of Attack,” AIAA-Paper 2009-3628, 2009.
  4. J. Boelens, “The blind-test activity of the GOAHEAD project”, 33rd European Rotorcraft Forum, Kazan, Russia, 2007.
  5. J. Boelens, H. van der Ven and J.C. Kok, “Rotorcraft simulations using a sliding-grid approach”, 34th European Rotorcraft Forum, Liverpool, UK, 2008.
  6. C. Kok, A Symmetry and Dispersion-Relation Preserving High-Order Scheme for Aeroacoustics and Aerodynamics, Proceedings ECCOMAS CFD 2006, ed. P. Wesseling and E. Onate and J. Periaux.
  7. C. Kok,A high-order low-dispersion symmetry-preserving finite-volume method for compressible flow on curvilinear grids,Journal of Computational Physics, Vol. 228, pp 6811-6832, 2008, also NLR-TP-2008-775.
  8. Kok, J. C., Computation of sound radiation from cylindrical ducts with jets using a high-order finite-volume method, AIAA paper 2007-3489, 13th AIAA/CEAS Aeroacoustics Conference, Rome, Italy, 21-23 May 2007, also NLR-TP-2007-514.
  9. C. Kok, H.S. Dol, B. Oskam, H. van der Ven,Extra-Large Eddy Simulation of Massively Separated Flows, AIAA paper 2004-264, 42nd AIAA Aerospace Sciences Meeting, Reno, 5-8 January 2004.
  10. C. Kok, B. I. Soemarwoto, H. van der Ven, Extra-Large Eddy Simulations Using a High-Order Finite-Volume Scheme, in Advances in Hybrid {RANS}-{LES} Modelling,Notes on Numerical Fluid Mechanics and Multidisciplinary Design, ed. S.H. Peng and W. Haase, vol. 97, pp 87-96, Springer, 2008, also NLR-TP-2007-800.
  11. C. Kok and H. van der Ven, Destabilizing free shear layers in X-LES using a stochastic subgrid-scale model,in Progress in Hybrid RANS-LES Modelling, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, ed. S.H. Peng and P. Doerffer and W. Haase, vol. 111, pp. 179-189, Springer, 2009, also NLR}-TP-2009-327.
  12. S. Dol, J.C. Kok, B. Oskam, Turbulence modelling for leading-edge vortex flows, AIAA paper 2002-0843, AIAA 40th Aerospace Sciences Meeting &; Exhibit, Reno, 14-17 January 2002.
  13. Kok, J.C. and Spekreijse, S. P., Efficient and accurate implementation of the k-w turbulence model in the NLR multi-block Navier-Stokes system, ECCOMAS 2000, Barcelona, Spain, 11-14 September 2004, also NLR-TP-2000-144.
  14. C. Kok,Resolving the dependence on freestream values for the k-w turbulence model, AIAA Journal, vol. 38, no. 7, pp. 1292-1294, 2000.
  15. I. Soemarwoto, M. Laban, A. Jameson, A. L. Martins and B. Oskam, “Adaptive aerodynamic optimization of regional jet aircraft”, AIAA-2002-260, AIAA Aerospace Sciences Meeting and Exhibit, 40th, Reno, NV, Jan. 14-17, 2002.
  16. Laban, B.I. Soemarwoto and J. Kooi, “Reshaping engine nacelles for testing in wind tunnels with turbofan propulsion simulators”, AIAA-2005-3703, 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, Arizona, July 10-13, 2005.
  17. I. Soemarwoto and A.B. Kloosterman, “Flow Characteristics around the Knife Edge of a Worn Labyrinth Seal revealed using Computational Fluid Dynamics”, presented at ETN 2008 4th International Conference, Brussels, 15-16 October 2008.
  18. J.G. Eussen and M.H.L. Hounjet. Aeroelastic analysis of a fighter type aircraft in a LCO-sensitive configuration. Paper presented at the RTO Applied Vehicle Technology Panel (AVT) Symposium held in Loen, Norway, on 5-8 May 2008.
  19. B. Prananta, M.H.L. Hounjet and B.J.G. Eussen Flutter analyses of fighter aircraft with metallic and hybrid metal-composite wings. Paper presented at International Forum on Aeroelasticity and Structural Dynamics IFASD-2009 in Seattle, USA, June 21-25, 2009. Also NLR-TP-2009-222.
  20. B. Prananta, R.P.G. Veul, R. Houwink, M.H.L. Hounjet and J. van Muijden. A generic flexible aircraft loads database system for fatigue analysis. Paper presented at International Forum on Aeroelasticity and Structural Dynamics 2007, Stockholm, 18-20 June 2007.Also NLR-TP-2007-381
  21. B. Prananta, A. Namer, H. Maseland, J. van Muijden and S. Spekreijse. Winglets on large civil aircraft: impact on wing deformation and flow characteristics. Paper presented at International Forum on Aeroelasticity and Structural Dynamics 2005, Munich, 18-20 June 2005.
  22. B. Prananta, B.I. Soemarwoto, O.J. Boelens, B.S. Kartika, S. Chaedar, Analysis of store separation from a generic twinengine turboprop aircraft, 25th AIAA Applied Aerodynamic Conference, June 25-28, 2007, Miami, FL, AIAA-2007-4077.