Mustangs and Tempests had it as standard, yet trials aircraft had it to such a degree that it required special manufacturing and handling techniques, the trials Hurricane fitting into the upper end of laminar cleanliness (higher Reynolds number). Laminar-flow technology of wings is one of those great subjects to debate, as there are so many variations in the technology. Trials were also carried out on an RAE Kingcobra RPS is correct with the AW info, from memory of seeing the pics I don't think the wings were that much different in plan from a standard Hurricane, the aerofoil shape, thickness/chord ratio, and cleanliness of the design and manufacture seemingly being the big issues. Haven't got specific info to hand, but have some somewhere that I will try and dig out. In: 5th Applied Aerodynamics Conference (1987) Tamigniaux, T.L.B., Stark, S.E., Brune, G.W.: An experimental investigation of the insect shielding effectiveness of a Krueger flap/wing airfoil configuration. Keller, D., Wild, J.: High-lift concepts compatible with laminar flow wings. Wild, J., Brezillon, J., Amoignon, O., Quest, J., Moens, F., Quagliarella, D.: Advanced design by numerical methods and wind tunnel verification within the European high-lift program. In: Deutsche Gesellschaft für Luft-und Raumfahrt (DGLR) (eds) DGLR-Jahrbuch 2001, vol. 3, pp. Heinze, W., Österheld, C.M., Horst, P.: Multidisziplinäres Flugzeugentwurfsverfahren PrADO-Programmentwurf und Anwendung im Rahmen von Flugzeug-Konzeptstudien. Seitz, A., Hübner, A., Risse, K.: Das DLR Projekt TuLam-Entwurf eines Flugzeugs mit vorwärts gepfeiltem Laminarflügel. Forschungsbericht 2001–2011, Institute of Aerodynamics and Flow Technology, German Aerospace Center, Braunschweig, Germany (2001) Wild, J.: Numerische Optimierung von zweidimensionalen Hochauftriebskonfigurationen durch Lösung der Navier-Stokes-Gleichungen. thesis, Department of Computer Sciences, University of Texas at Austin, Austin, Texas, USA (1990) Rowan, T.: Functional stability analysis of numerical algorithms. volume 1 of Aerospace Science and Technology, pp. Spalart, P.R., Shur, M.: On the sensitization of turbulence models to rotation and curvature. Spalart, P.R., Allmaras, S.R.: A one-equation turbulence model for aerodynamic-flows. In: MEGAFLOW-Numerical Flow Simulation for Aircraft Design, volume 89 of Notes on Numerical Fluid Mechanics and Multidisciplinary Design, pp. Gerhold, T.: Overview of the hybrid RANS code TAU. In: MEGAFLOW-Numerical Flow Simulation for Aircraft Design. Raddatz, J., Fassbender, J.K.: Block structured Navier–Stokes solver FLOWer. volume 132 of Notes on Numerical Fluid Mechanics and Multidisciplinary Design, pp. In: 29th Congress of the International Council of the Aeronautical Sciences (2014)įranke, D., Wild, J.: Aerodynamic Design of a Folded Krüger Device for a HLFC Wing. Strüber, H., Wild, J.: Aerodynamic Design of a High-Lift System Compatible with a Natural Laminar Flow Wing within the DeSiReH Project. In: 5th European Conference for Aeronautics and Space Sciences (EUCASS) (2013) Iannelli, P., Wild, J., Minervino, M., Strüber, H., Moens, F., Vervliet, A.: Design of a High-Lift System for a Laminar Wing. Wild, J.: Overview on the DeSiReH Project. designed the mustang to be low drag the wings may have been designed to be laminar flow but from what I have read this was not achieved it requires surface cleanliness and smoothness not achievable on a combat aircraft in service. Contractor Report CR-1999-209324, NASA (1999) Laminar Flow Airfoil Some interesting stuff on the above link. Contractor Report 4746, NASA (1996)īoeing Commercial Airplane Group: High Reynolds Number Hybrid Laminar Flow Control (HLFC) Flight Experiment II. Rudolph, P.K.C.: High-Lift Systems on Commercial Subsonic Airliners. In: 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition Number 22 (1993)īright, M., Korntheuer, A., Komadina, S., Lin, J.: Development of advanced high lift leading edge technology for laminar flow wings. Walchli, L.A.: High Lift and the Forward Swept Wing.
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