1. 80 -13.00 Cy 1inder 2.56 -1.30 Flat Plate 4.00 - 2.60 Flat Plate 3.80 10.20 Cy 1i nder 2.56 10.30 Flat Plate 4.00 12.80 Flat Plate 2.56 9.52 Fl?t Plate 4.00 15.92 Flat Plate 2.56 - 4.60 Flat Plate 4.00 - 7.80 Flat Plate 2.56 8.60 Flat Plate 4.00 10.34 Flat Plate 7.00 100.00 Flat Plate 2.56 10.20 Flat Plate 4.00 16.00 Flat Plate 2.56 21.00 Flat Plate 4.00 33.00 Flat Plate 3.80 29.60 Cylinder 2.56 6.10 Flat Plate 4.00 13.20 Flat Plate 2.56 5.10 Flat Plate 4.00 9.20 Flat Plate 2.56 11.70 Flat Plate 4.00 21.20 Flat Plate 2.56 18.00 Flat Plate 4.00 21 .oo Flat Plate 2.56 -14.60 Flat Plate 4.00 -29.20 Flat Plate 2.56 47.00 Flat Plate 4.00 91.20 Flat Plate
2. With the substitution of equation (31, the energy thickness takes the form (x/C > 0.4), 62 - 251., The detailed discussion of energy thickness i s given i n Reference 13. The energy thickness increases with the increase i n free stream turbulence at zero pressure gradient.
3. 'Pal, S."Wake Boundary Layer Interaction i n Turbomachinery," Ph.D. Thesis, Department of Mechanical Enqineerinq. The Citv Colleqe of theCity University of New York, Miy1981: