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Master Thesis Report Bibliography Bibliography [1] A.P. Plas, M.A. Sargeant, V. M. D. E. G. and Hynes, T., “Performance of a Boundary Layer Ingesting Propulsion System,” AIAA 2007-0450, January 2007. [2] Drela, M., “Power Balance Method in Aerodynamic Flows,” AIAA 2009-3762, June 2009. [3] Drela, M., “MIT, Aurora Flight Sciences, Pratt and Whitney, and NASA. Aircraft and Technology Concepts for an N+3 Subsonic Transport - Phase 2,” Year 3 Status Review Presentation, February 2014. [4] Hanlon, C., “Engine Design Implication for a Blended Wing-Body Aircraft with Boundary Layer Ingestion,” Tech. rep., Master Thesis, Department of Aeronautics and Astronautics, 2010. [5] Boxer, E., “Influence of wall boundary layer upon the performance of an axial flow fan rotor,” NASA Langley Research Center, Technical Report TN-2291, February 1951. [6] Kimzey, W., “An analysis of the influence of some external disturbance on the aerodynamic stabil- ity of turbine engine axial flow fans and compressor,” Tech. rep., Arnold Engineering Development Center, Arnold Airforce Station, 1977. [7] R.C.W.de.Koning, “Development of a Parametric 3D Turbomachinery Blade Modeller,” Tech. rep., Master Thesis, Faculty of Aerospace Engineering, Delft University of Technology, 2015. [8] Verstraete, T., “CADO: A Computer Aided Design and Optimization Tool for Turbomachinery Applications,” 2nd International Conference on Engineering Optimization, VKI , September 2010. [9] Verabhi, “Secondary Flow Losses,” https://en.wikipedia.org/wiki/File:Secondary_flow_ losses.png, 2013, [Online; accessed 03-August-2015]. [10] Dixon, S. and C.A.Hall, Fluid Mechanics and Thermodynamics of Turbomachinery, Elsevier, 6th ed., 2010. [11] Ferrar, A. and O’Brien, W., “Progress in Boundary Layer Ingesting Embedded Engine Research,” AIAA 2012-4283, August 2012. [12] H.J.M. Kok, M. V. and van Tooren, M. J., “Distributed Propulsion featuring Boundary Layer Ingestion Engines for the Blended Wing Body Subsonic Transport,” AIAA 2010-3064 , April 2010. [13] Francisco Palacios, Michael R. Colonno, A. C. A. A. C. S. R. C. T. D. E. A. K. L. T. W. L. T. W. T., “Stanford University Unstructured (SU2): An open-source integrated computational environment for multi-physics simulation and design,” AIAA 2013-0287, January 2013. [14] Medida, S. and Baeder, J., “Numerical prediction of static and dynamic stall phenomenon using the γ − Reθt model,” American Helicopter Society 67th Annual Forum, May 2011. IPDF Image | Aerodynamic Design of the NASA Rotor 67 for Non Uniform Inflow
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