% Top wall pressure, weak shock case % % H* = Throat height % P0 = Inlet total pressure % X/H* P/P0 -4.035 .86358 -3.389 .86323 -2.755 .87110 -2.029 .88016 -1.706 .82975 -1.037 .66436 -0.749 .59615 -0.473 .55702 -0.288 .54251 -0.144 .54397 0.000 .53958 0.144 .53467 0.288 .52326 0.438 .50449 0.553 .48068 0.692 .46266 0.830 .45219 0.991 .43329 1.130 .41878 1.280 .40884 1.418 .50016 1.556 .56901 1.787 .60727 2.006 .63078 2.225 .65319 2.444 .67167 2.882 .70519 3.314 .73280 3.977 .76504 4.403 .77972 5.101 .79741 5.764 .80906 6.340 .81371 6.916 .81536 7.493 .81687 8.069 .81817 8.646 .82121