{"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":"3c45902c-b918-5ed2-b321-40eb8db2fadc","task_key":"default--test--11456","task_revision_id":"1","upstream_id":"11456","short_description":"Air flowing through a nozzle encounters a shock. The Mach number upstream of the…","config":"default","split":"test","body":"{\"category\":\"engineering\",\"options\":\"['1300 ft/sec', '1230 ft/sec', '950 ft/sec', '1160 ft/sec', '1050 ft/sec', '1200 ft/sec', '1100 ft/sec', '1500 ft/sec', '1400 ft/sec', '880 ft/sec']\",\"question\":\"Air flowing through a nozzle encounters a shock. The Mach number upstream of the shock isM_x= 1.8, and the static temperature downstream of the shock is T_y = 800°R. How much has the velocity changed across the shock ? Assume \\\\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":[]}