{"kind":"task","effective_mode":"full","benchmark":{"kind":"benchmark","effective_mode":"full","slug":"mmlu-pro","formal_name":"MMLU-Pro","introduction":"MMLU-Pro rebuilds MMLU with ten answer options instead of four and removes items that no longer separate models. Questions span fourteen academic and professional subjects.","introduction_ja":"","introduction_en":"","category":"Category not supplied","task_count":null,"acquisition_status":"Acquisition status not supplied","official_url":"https://huggingface.co/datasets/TIGER-Lab/MMLU-Pro","indexing_mode":"index","profile":{"resources":[],"task_format":"","scoring":"","metric":"","size":"","answer_access":"","license":"","citation":"","maintainer":"","released":"","why_hard":"","related":[],"history":"","construction":"","limitations":"","saturation":"","scores":[]}},"task_id":"3a31b915-7ab2-530e-bdab-c467b889b42d","task_key":"default--test--11827","task_revision_id":"1","upstream_id":"11827","short_description":"The pressure and Mach number of helium flowing through a channelat a certain…","config":"default","split":"test","body":"{\"category\":\"engineering\",\"options\":\"['2.80', '1.65', '0.75', '1.98', '2.05', '2.5', '1.25', '0.50', '0.124', '1.5']\",\"question\":\"The pressure and Mach number of helium flowing through a channelat a certain point are found to be P = 30psiaand M = 1.5. At a point further downstream the pressure is 15psia.Assuming isentropic flow through the channel, determinethe Mach number at the second point. Assume \\\\gamma = 1.67. One-Dimensional Isentropic Compressible-Flow Functions For an ideal gas with constant specific heat and molecular weight, \\\\gamma = 1.67 M (A/A\\\\textasteriskcentered) (P/P_0) M (A/A\\\\textasteriskcentered) (P/P_0) 0 \\\\infty 1.0000 1.75 1.312 0.1721 0.05 11.265 0.9979 1.80 1.351 0.1601 0.10 5.661 0.9917 1.85 1.392 0.1490 0.15 3.805 0.9815 1.90 1.436 0.1386 0.20 2.887 0.9674 1.95 1.482 0.1290 0.25 2.344 0.9497 2.00 1.530 0.1201 0.30 1.989 0.9286 2.05 1.580 0.1119 0.35 1.741 0.9046 2.10 1.632 0.1042 0.40 1.560 0.8780 2.15 1.687 0.09712 0.45 1.424 0.8491 2.20 1.744 0.09053 0.50 1.320 0.8184 2.25 1.803 0.08442 0.55 1.239 0.7862 2.30 1.865 0.07875 0.60 1.176 0.7529 2.35 1.929 0.07349 0.65 1.126 0.7190 2.40 1.995 0.06862 0.70 1.0874 0.6847 2.45 2.064 0.06410 0.75 1.0576 0.6503 2.50 2.135 0.05990 0.80 1.0351 0.6162 2.55 2.209 0.05601 0.85 1.0189 0.5826 2.60 2.285 0.05239 0.90 1.0080 0.5497 2.65 2.364 0.04903 0.95 1.0019 0.5177 2.70 2.445 0.04591 1.00 1.0000 0.4867 2.75 2.529 0.04301 1.05 1.0018 0.4568 2.80 2.616 0.04032 1.10 1.0071 0.4282 2.85 2.705 0.03781 1.15 1.0154 0.4009 2.90 2.797 0.03547 1.20 1.0266 0.3749 2.95 2.892 0.03330 1.25 1.0406 0.3502 3.0 2.990 0.03128 1.30 1.0573 0.3269 3.5 4.134 0.01720 1.35 1.0765 0.3049 4.0 5.608 0.009939 1.40 1.0981 0.2842 4.5 7.456 0.006007 1.45 1.122 0.2647 5.0 9.721 0.003778 1.50 1.148 0.2465' 6.0 15.68 165(10)^-5 1.55 1.176 0.2295 7.0 23.85 807(10)^-6 1.60 1.207 0.2136 8.0 34.58 429(10)^-6 1.65 1.240 0.1988 9.0 48.24 244(10)^-6 1.70 1.275 0.1850 10.0 65.18 147(10)^-6 \\\\infty \\\\infty 0\",\"src\":\"stemez-FluidMechanics\"}","display_format":"text","language":"","answer_status":"published","assets":[],"source_url":"https://huggingface.co/datasets/TIGER-Lab/MMLU-Pro","history":"initial import","indexing_mode":"index","subproblems":[],"grids":[]}