{"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":"a19e1492-761f-5305-a1d3-1396b1151f8e","task_key":"default--test--11362","task_revision_id":"1","upstream_id":"11362","short_description":"Air is flowing through a nozzle with a 90% efficiency and an expansion rate of…","config":"default","split":"test","body":"{\"category\":\"engineering\",\"options\":\"['Exit area = 2.37 × 10^-3m^2, Velocity = 550 m/s, Enthalpy = 400 KJ/kg', 'Exit area = 5.37 × 10^-3m^2, Velocity = 850 m/s, Enthalpy = 550 KJ/kg', 'Exit area = 6.37 × 10^-3m^2, Velocity = 900 m/s, Enthalpy = 610 KJ/kg', 'Exit area = 3.37 × 10^-3m^2, Velocity = 658 m/s, Enthalpy = 465.8 KJ/kg', 'Exit area = 4.97 × 10^-3m^2, Velocity = 800 m/s, Enthalpy = 480 KJ/kg', 'Exit area = 3.87 × 10^-3m^2, Velocity = 620 m/s, Enthalpy = 560 KJ/kg', 'Exit area = 2.97 × 10^-3m^2, Velocity = 700 m/s, Enthalpy = 520 KJ/kg', 'Exit area = 1.37 × 10^-3m^2, Velocity = 600 m/s, Enthalpy = 580 KJ/kg', 'Exit area = 4.37 × 10^-3m^2, Velocity = 750 m/s, Enthalpy = 500 KJ/kg', 'Exit area = 2.77 × 10^-3m^2, Velocity = 780 m/s, Enthalpy = 530 KJ/kg']\",\"question\":\"Air is flowing through a nozzle with a 90% efficiency and an expansion rate of 2.0 Kg/s. The inlet conditions are P = 550kPa and T = 680°K. If the exit pressure is 120kPa calculate the actual exit area, velocity and enthalpy. Assume K = 1.4.\",\"src\":\"stemez-Thermodynamics\"}","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":[]}