Concepts
Equation
Math
Graphs
Mystery
100

NPSHa < NPSHr is acceptable from pump operation (T/F)

False: a pump requires a certain amount of head at the inlet to operate, so if the actual in the system is lower, the pump will cavitate

100

The Equation for calculating brake horsepower for a pump

BHP = (hydraulic hp)/(pump efficiency)

100

Determine the overall outer heat transfer coefficient given:

pipe: 15 [m]

ri = 5[cm] t = 3 [cm]

hi = 2500 [W/m2 C]          ho = 7 [W/m2 C]

ksteel = 43 [W/m C]


1.722 [W/m2 C]

100

temperature inlet/outlet diagram for an AFU where:

T,tube, in = 377 [F]

T,tube,out = 200 [F]

Tshell, in = 160 [F]

Tshell, out = 275 [F]

*SoMe DrAwInG ReQuIrEd*

100

Delta P equation as a function of hydraulic head

delta P = (head [ft] * specific gravity)/2.31

200

The methods and mediums of convection and conduction in a system

Convection: what is fluid flow across a solid in the boundary layer

Conduction: What is molecular interactions throughout a solid

200

Equation for annual operating cost

annual operating cost = (utility amount)(cost per amount)

200

NPSHa acceptable for the system provided for propane at its bubble point at 100 [F] given: specific gravity = 0.485, NPSHr = 10 [ft]

losses:

check valve = 1.0 [psi]             valves = 0.2 [psi]

orifice = 1.2 [psi]                   control valve = 9 [psi]

line losses = 0.75 [psi]


NPSHa = 24.04 [ft], Yes 

200

The graphical representation of co-current and counter-current H.E (w' no phase change) and their thermodynamically impossible graphs

*insert drawings of pretty graphs here*

200

The point at which the max. flowrate occurs for compressed flow

when is the choked point/in choked flow

300

The effect of relative roughness on the friction factor within laminar flow

What is no effect

(see Moody diagram)

300

equation for radiative heat transfer

q1-2 = (sigma)A(F12)((T1^4)-(T2^4))

300

hydraulic hp required for a pump moving liquid propane 

specific gravity = 0.485

Q  = 375 [gpm]

Psuction = 175 [psig]          Pdischarge = 260 [psia]

15.4 [hp]

300

Illustrate heat transfer from a 80 [F] space through a layer of steel sandwiched between layers of insulation to a freezer at -20[F]

show the pretty picture with all labels and visual aids

300

Moody and Fanning friction factor are equivalent and completely interchangeable (T/F)

They can be used in the same scenario but Fanning = 1/4 Moody and have different equations and graphs

400

type of convection with largest heat transfer coefficient

forced convection

400

Equation for flowrate through nozzle

Q = Cn*An*SQRT((2(p1-p2))/(density(1-beta^4))))

400

q/L for pipe w' Ts = 176[F], ro = 1.35 [in] with air @ velocity = 70 [ft/s], Patm and 110 [F] flowing across it given:

viscosity air = 0.021 [lbm/ft h]

density air = 0.0613 [lbm/ft^3]

air thermal conductivity = 0.0181 [Btu/(h ft F)]

q/L = 45.03 [Btu/h ft]

400

Find q subcooled based on graph given:

mh = 10 [lbm/h]                  mc = 15 [lbm/h]

Cp,h = 6.65 [Btu/lbm F]       Cp,c = 1 [Btu /lbm F]

hfg,h (or lambda,h) = -812 [Btu/lbm]          

hfg, c (or lamba,c) = -615 [Btu/lbm]

q subcooled = 1915 [Btu/h]

400

heat removed during phase change

what is latent heat?

500

the two assumptions inherent to assuming isentropic nozzle compressed flow

what are reversible and adiabatic

500

Demonstrate whether heat flux is conserved in cylindrical and planar conduction geometries

This is a bit *DiFfIcUlT* to type; see board

500

Using the Lockhart-Martinelli Method, the delta P(two-phase) over 347[ft] of 5[in] inner diameter pipe assuming plug flow regime:

                                 Vapor                    Liquid

density [lbm/ft^3]       2.43                     29.49

viscosity [cP]            1.021*10^-2       5.365*10^-2

surface tension [dyne/cm]                        4.62

mass flowrate [lbm/h]   2500                    2000

1159 [psi]

500

Given the pump curve shown, what is the pressure added by the pump handling a flowrate of 500[gpm] and 11[in] impeller if the fluid has a specific gravity of 0.847.

 18.33 [psi]

500

Given the wall shown with the specifications, what is the temperature at the interface between wall 2 and 3?

T = 286.3 [K]