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For a laminar flow of air (Pr = 0.71) over a flat plate at zero incidence, the thickness of the velocity boundary layer 8 and the hydrodynamic boundary layer δt are such that
  • a)
    δ > δ
  • b)
    δt = δ
  • c)
    δt < δ
  • d)
Correct answer is option 'A'. Can you explain this answer?
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For a laminar flow of air (Pr = 0.71) over a flat plate at zero incidence, the thickness of the velocity boundary layer 8 and the hydrodynamic boundary layer δtare such thata)δt > δb)δt = δc)δt < δd)Correct answer is option 'A'. Can you explain this answer?
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For a laminar flow of air (Pr = 0.71) over a flat plate at zero incidence, the thickness of the velocity boundary layer 8 and the hydrodynamic boundary layer δtare such thata)δt > δb)δt = δc)δt < δd)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 For a laminar flow of air (Pr = 0.71) over a flat plate at zero incidence, the thickness of the velocity boundary layer 8 and the hydrodynamic boundary layer δtare such thata)δt > δb)δt = δc)δt < δd)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 For a laminar flow of air (Pr = 0.71) over a flat plate at zero incidence, the thickness of the velocity boundary layer 8 and the hydrodynamic boundary layer δtare such thata)δt > δb)δt = δc)δt < δd)Correct answer is option 'A'. Can you explain this answer?.
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