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AERO4140 - Aerodynamics III - QUIZ

AERO4140 · Aerodynamics III

Auburn University

Questions
28 Questions

Practice 28 questions on AERO4140 - Aerodynamics III at Auburn University. Free AI-generated quiz on uNotes — track your score, retake anytime.

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Questions

  1. 1According to the von Karman integral momentum approach for a flat plate boundary layer, the wall shear stress is proportional to the rate of change of which boundary layer property?
  • 2For a laminar incompressible flow over a flat plate with a linear velocity profile (u/U = y/delta), what is the ratio of displacement thickness to boundary layer thickness (delta*/delta)?
  • 3Which of the following conditions must be satisfied for a flow to be considered mathematically incompressible based on its velocity vector V?
  • 4Pohlhausen (1921) proposed five boundary conditions for the velocity profile u(y) to ensure smooth merging with the freestream. Which of the following are included in those five conditions?
  • 5In a laminar pipe flow with a parabolic velocity profile u = u_max * [1 - (r/R)^2], what is the value of the kinetic energy correction factor (alpha)?
  • 6If a flow field is defined by the velocity vector V = 2xt i - 2yt j, what is the magnitude of the acceleration at the point (2, 2) at time t = 0?
  • 7In Pohlhausen's quartic polynomial analysis for flow over a flat plate, flow separation occurs when the pressure gradient parameter (Lambda) reaches what value?
  • 8When comparing a turbulent boundary layer (1/7th power law) to a laminar boundary layer on a flat plate, which statement is true regarding the shape factor H = delta*/theta?
  • 9Dimensional analysis of the pressure drop (delta p) across a pipe contraction involving variables rho, mu, V, D1, and D2 results in how many independent dimensionless Pi groups?
  • 10Which of the following describes the 'no-slip' condition in aerodynamics?
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