[1] B. Lakshminarayana and J. H. Horlock, Leakage and Secondary Flows in Compressor Cascades, Ministry of Technology Aeronautical Research Council Report and Memoranda, No. 3483, 1987.
[2] P. Merati, H. M. McMahon and K. M. Yoo, Experimental investigation of a turbulent flow in the vicinity of an appendage mounted on a flat plate, J. Fluids Eng. 113(4) (1991), 635-642.
[3] A. K. Abdulla, R. K. Bhargava and R. Raj, An experimental study of local wall shear stress, surface statics pressure, and flow visualization upstream, alongside, and downstream of a blade endwall corner, J. Turbomach. 113 (1991), 626-632.
[4] C. B. Steenaert, B. W. van Oudheusden and L. M. M. Boermans, Simple Approach for the Design of a Wing Body Fairing, CEAS Aerospace Aerodynamics Research Cambridge, U.K., 2002.
[5] M. Tobak and D. J. Peake, Topology of three dimensional separated flow, NACA Technical Report, 1982.
[6] H. Schlighting, Boundary Layer Theory, 4th ed., McGraw-Hill, Washington DC, 1962.
[7] M. J. Serry, D. L. Jacono and J. Sheridan, Flow separation characterisation of a forward facing step immersed in a turbulent boundary layer, Sixth International Symposium of Turbulence and Shear Flow Phenomena, Seoul, Korea, 22-24 June, 2009.
[8] R. L. Maltby, Flow Visualization in Wind Tunnels Using Indicators, AGARDograph No. 70. (1962).
[9] H. Mirmanto, Sutrisno, H. Sasongko and D. Z. Noor, Reduction of energy loss in endwall junction area through the addition of forward facing step turbulent generator, Appl. Mech. Mater. 493 (2014), 256-261.
[10] Fox dan McDonald’s, Introduction to Fluid Mechanics, 8th ed., John Willey & Sons, Inc., 2011.
[11] D. B. De Graaff and J. K. Eaton, Reynolds-number scaling of the flat-plate turbulent boundary layer, J. Fluid Mech. 422 (2000), 319-346. |