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Consider a laminar boundary layer over a heated flat plate. The free stream velocity is U∝. At some distance x from the leading edge the velocity boundary layer thickness is δv and the thermal boundary layer thickness is δT. If the Prandtl number is greater than 1, then[2003]a)δv > δTb)δT > δvc)d)Correct answer is option 'A'. Can you explain this answer? for Mechanical Engineering 2024 is part of Mechanical Engineering preparation. The Question and answers have been prepared according to the Mechanical Engineering exam syllabus. Information about Consider a laminar boundary layer over a heated flat plate. The free stream velocity is U∝. At some distance x from the leading edge the velocity boundary layer thickness is δv and the thermal boundary layer thickness is δT. If the Prandtl number is greater than 1, then[2003]a)δv > δTb)δT > δvc)d)Correct answer is option 'A'. Can you explain this answer? covers all topics & solutions for Mechanical Engineering 2024 Exam. Find important definitions, questions, meanings, examples, exercises and tests below for Consider a laminar boundary layer over a heated flat plate. The free stream velocity is U∝. At some distance x from the leading edge the velocity boundary layer thickness is δv and the thermal boundary layer thickness is δT. If the Prandtl number is greater than 1, then[2003]a)δv > δTb)δT > δvc)d)Correct answer is option 'A'. Can you explain this answer?.

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