{"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":"1049e0e2-c027-5f0c-8986-78196a82fc4a","task_key":"default--test--11990","task_revision_id":"1","upstream_id":"11990","short_description":"A supersonic wind-tunnel consists of a large reservoir containing gas under high…","config":"default","split":"test","body":"{\"category\":\"engineering\",\"options\":\"['4000 mm^2', '4900 mm^2', '7500 mm^2', '5000 mm^2', '3500 mm^2', '4500 mm^2', '5360 mm^2', '6000 mm^2', '6800 mm^2', '6200 mm^2']\",\"question\":\"A supersonic wind-tunnel consists of a large reservoir containing gas under high pressure which is discharged through a convergent-divergent nozzle to a test section of constant cross-sectional area. The cross-sectional area of the throat of the nozzle is 500 mm^2 and the Mach number in the test section is 4. Calculate the cross-sectional area of the test section assuming \\\\gamma = 1.4.\",\"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":[]}