A. 0.1
B. 0.01
C. 0.001
D. 0.0001
A. 0.1
B. 0.01
C. 0.001
D. 0.0001
A. a circular disc or plate held normal to flow
B. a sphere
C. a cylinder
D. an airfoil
A. highest intensity of pressure occurs around the circumference at right angles to flow
B. lowest pressure intensity occurs at front stagnation point
C. lowest pressure intensity occurs at rear stagnation point
D. total drag is zero
A. log-log plot of friction factor against Reynolds number
B. log-log plot of relative roughness against Reynolds number
C. semi-log plot of friction factor against Reynolds number
D. semi-log plot of friction factor against relative roughness
A. velocity
B. discharge
C. head
D. pressure
A. x”7
B. x,/2
C. x4/5
D. x3/5
where x is the distance from leading edge
A. constant over the cross section
B. parabolic distribution across the section
C. zero at the mid plane and varies linearly with distance from mid plane
D. zero at plates and increases linearly to midpoint
A. H1/2
B. H3/2
C. H5/2
D. H
where H is head
A. 1.00
B. 0.855
C. 0.7H
D. 0.611
A. slightly less
B. slightly more
C. nearly half
D. equal