Experimental data from Hseih, Wardlaw, Collins and Coakely, (1987), "Numerical Investigation of Unsteady Inlet Flowfields," AIAA Journal, Vol. 25, No. 1, January 1987, pp. 75-81. The tabulated data listed below is taken from a data file received from the authors. All distances have been normalized with the throat height, H = 0.14435 ft = 4.407 cm. SURFACE STATIC PRESSURE ----------------------- TOP WALL BOTTOM WALL X/H* P/P0 X/H* P/P0 -4.035 .86358 -4.035 .86040 -3.389 .86323 -3.386 .85840 -2.755 .87110 -2.487 .84544 -2.029 .88016 -2.017 .81856 -1.706 .82975 -1.695 .78999 -1.037 .66436 -0.937 .67503 -0.749 .59615 -0.761 .64874 -0.473 .55702 -0.455 .58480 -0.288 .54251 -0.288 .56893 -0.144 .54397 -0.110 .56395 0.000 .53958 0.000 .55086 0.144 .53467 0.147 .53661 0.288 .52326 0.401 .52723 0.438 .50449 0.562 .50163 0.553 .48068 0.700 .49769 0.692 .46266 0.841 .47210 0.830 .45219 0.983 .45553 0.991 .43329 1.127 .44105 1.130 .41878 1.271 .42924 1.280 .40884 1.415 .49445 1.418 .50016 1.559 .57634 1.556 .56901 1.790 .61770 1.787 .60727 2.020 .64190 2.006 .63078 2.239 .65916 2.225 .65319 2.452 .67619 2.444 .67167 2.885 .70596 2.882 .70519 3.320 .72967 3.314 .73280 3.983 .75893 3.977 .76504 4.383 .77172 4.403 .77972 5.075 .78969 5.101 .79741 5.767 .80117 5.764 .80906 6.343 .80757 6.340 .81371 6.919 .81294 6.916 .81536 7.496 .81486 7.493 .81687 8.073 .81695 8.069 .81817 8.649 .82192 8.646 .82121 VELOCITY PROFILES ----------------- X/H = 1.729 Y/H X-VELOCITY M/S 0.012 121.21 0.023 161.83 0.035 199.17 0.046 234.86 0.058 268.91 0.069 278.53 0.086 284.76 0.115 284.63 0.144 285.10 0.173 284.43 0.231 282.90 0.288 282.23 0.346 280.89 0.432 278.71 0.494 280.75 0.552 280.11 0.609 280.35 0.667 280.95 0.724 281.28 0.782 282.35 0.840 283.72 0.897 285.31 0.926 285.18 0.955 279.59 0.984 277.53 1.013 264.80 1.036 192.78 1.047 147.22 1.059 98.56 X/H = 2.882 Y/H X-VELOCITY M/S 0.012 90.79 0.023 110.98 0.035 129.64 0.046 147.80 0.058 167.50 0.069 183.70 0.086 208.95 0.115 238.43 0.144 241.91 0.173 242.05 0.231 242.41 0.288 241.08 0.346 240.93 0.432 241.00 0.556 239.92 0.614 241.14 0.671 240.92 0.729 239.68 0.787 240.24 0.844 240.59 0.902 239.36 0.960 240.44 1.017 239.89 1.046 238.96 1.075 233.96 1.104 215.58 1.133 175.97 1.161 128.70 1.179 102.92 X/H = 4.611 Y/H X-VELOCITY M/S 0.012 75.27 0.023 85.12 0.035 92.36 0.046 100.57 0.058 108.91 0.069 117.47 0.086 130.05 0.115 150.72 0.144 170.62 0.173 187.05 0.231 203.82 0.288 206.77 0.346 205.87 0.432 205.83 0.492 206.06 0.607 204.23 0.723 203.49 0.838 202.57 0.953 202.27 1.069 202.23 1.126 201.54 1.184 195.64 1.241 168.96 1.270 147.29 1.299 125.56 1.328 105.11 1.357 86.52 1.386 71.13 1.403 57.74 X/H = 6.340 Y/H X-VELOCITY M/S 0.012 77.68 0.023 87.87 0.035 91.60 0.046 97.03 0.058 102.45 0.069 106.62 0.086 111.47 0.115 124.87 0.144 137.12 0.173 151.03 0.231 173.16 0.288 184.27 0.346 188.52 0.432 189.02 0.588 188.18 0.703 187.71 0.818 187.26 0.934 186.12 1.049 185.57 1.164 184.15 1.222 176.94 1.280 159.71 1.337 135.26 1.366 123.26 1.395 111.37 1.424 99.82 1.452 89.49 1.481 80.26 1.499 69.10