Sail E0 Webinar

MCQs

Total Questions : 47 | Page 2 of 5 pages
Question 11. For a particular engine, the underside of the crankcase can be idealized as a flat plate measuring 80 cm by 20 cm. The engine runs at 80 km/hr and the crankcase is cooled by the air flowing past it at the same speed. Find loss of the heat from the crank case surface (t S = 25 degree Celsius). Assume the boundary layer to be turbulent
  1.    465.04 W
  2.    565.04 W
  3.    665.04 W
  4.    765.04 W
 Discuss Question
Answer: Option B. -> 565.04 W
Answer: (b).565.04 W
Question 12. A flat plate 1 m by 1 m is placed in a wind tunnel. The velocity and temperature of free stream air are 80 m/s and 10 degree Celsius. The flow over the whole length of the plate is made turbulent by turbulizing grid placed upstream of the plate. Find the heat flow from the surface of the plate
  1.    9424.5 W
  2.    8424.5 W
  3.    7424.5 W
  4.    6424.5 W
 Discuss Question
Answer: Option C. -> 7424.5 W
Answer: (c).7424.5 W
Question 13. The concept of hydrodynamic boundary layer was first suggested by
  1.    Isaac Newton
  2.    Ludwig Prandtl
  3.    Rodridge
  4.    Fourier
 Discuss Question
Answer: Option B. -> Ludwig Prandtl
Answer: (b).Ludwig Prandtl
Question 14. The pattern of flow in the boundary layer is judged by the
  1.    Reynolds number
  2.    Fourier number
  3.    Peclet number
  4.    Grashof number
 Discuss Question
Answer: Option A. -> Reynolds number
Answer: (a).Reynolds number
Question 15. The conditions for flow beyond the boundary layer and its outer edge are
  1.    d u/d y = 0 and u = U 0
  2.    d u/d y = Infinity and u = U INFINITY
  3.    d u/d y = 1 and u = U 0
  4.    d u/d y = 0 and u = U INFINITY
 Discuss Question
Answer: Option D. -> d u/d y = 0 and u = U INFINITY
Answer: (d).d u/d y = 0 and u = U INFINITY
Question 16. The free stream undisturbed flow has a uniform velocity U INFINITY in the
  1.    X-direction
  2.    Y-direction
  3.    Z-direction
  4.    Any direction
 Discuss Question
Answer: Option A. -> X-direction
Answer: (a).X-direction
Question 17. The thin layer where velocity changes continuously is called
  1.    Differential layer
  2.    Thermal boundary layer
  3.    Hydrodynamic boundary layer
  4.    Velocity distribution layer
 Discuss Question
Answer: Option C. -> Hydrodynamic boundary layer
Answer: (c).Hydrodynamic boundary layer
Question 18. A plate 0.3 m long is placed at zero angle of incidence in a stream of 15 degree Celsius water moving at 1 m/s. Find out the stream wise velocity component at the mid-point of the boundary layer. For water at 15 degree Celsius
p = 998.9 kg /m³
µ = 415.85 * 10¯² kg/hr m
  1.    0.736 m/s
  2.    0.636 m/s
  3.    0.536 m/s
  4.    0.436 m/s
 Discuss Question
Answer: Option A. -> 0.736 m/s
Answer: (a).0.736 m/s
Question 19. Shear stress at the middle of the plate is given by
  1.    T W = 0.964 p U INFINITY²/2 (Re)^1/2
  2.    T W = 0.864 p U INFINITY²/2 (Re)^1/2
  3.    T W = 0.764 p U INFINITY²/2 (Re)^1/2
  4.    T W = 0.664 p U INFINITY²/2 (Re)^1/2.
 Discuss Question
Answer: Option D. -> T W = 0.664 p U INFINITY²/2 (Re)^1/2.
Answer: (d).T W = 0.664 p U INFINITY²/2 (Re)^1/2.
Question 20. Local skin friction coefficient is given by
  1.    0.646/ (Re)^1/2
  2.    1.646/ (Re)^1/2
  3.    2.646/ (Re)^1/2
  4.    3.646/ (Re)^1/2
 Discuss Question
Answer: Option A. -> 0.646/ (Re)^1/2
Answer: (a).0.646/ (Re)^1/2

Latest Videos

Latest Test Papers