2. Background
• Disclaimer
• Pipe smoked non-traditionally for mathematical purposes
Bowl never removed for consistent, laminar flow
No water added so smoke is internal fluid
3. Introduction
• The objective of this study is to determine the temperature at which smoke
reaches the human body for 2 scenarios:
Forced internal convection with constant surface temp and constant convection at
surface
Internal fluid = smoke, external = air
• Constant surface temp: Freeze pipe and bring to equilibrium
Ts = Tfreezer
• Constant convection: Run fan over pipe during smoking process
4. Materials
• 49.1 cm tall cylindrical pipe (or any that can achieve fully developed thermal
flow)
• Viable thermometer
Mine rated for -50 C to 300 C
• Ruler
• Protractor
• Hemp
• Strobe tachometer
Mine was an iOS app
• Bladed fan
• Freezer/fridge
5. Methods
• Approximate pipe as 2 cylinders: pipe 1 = stem, pipe 2 = main chamber
• Scenario 1: constant heat flux at surface
Attach thermometer to entrance of stem
Run fan over pipe
Measure temperature of smoke entering stem
• Scenario 2: constant surface temperature
Freeze pipe
Measure temperature of smoke entering stem
6. Methods Cont.
• Mathematically determine temperature of smoke leaving pipe 2
• Temperature of mass entering pipe 2 = temperature of mass leaving pipe 1
8. Thermal Fully Developed Region
• Measure pipe dimensions
D
L
• Measure fan dimensions
rmax = 10.5 cm
rmin = 2.25 cm
θblade = 50°
• Using Re < 2300 for laminar flow
Thermal fully developed region occurs when x/D ≥ .05ReDPr
• Q = V/t
• u = Q/A
9. Proving Fully Developed Flow
• Calculate Re = uD/ϒ
Both were less than 2300
Showed that flow was indeed laminar as hypothesized
• Calculate Pr = ϒ/α
Showed that flow was thermal fully developed flow
10. Condition 1: Constant Convection at
Surface
• Find Nu = 4.36 = hD/kf
Use to solve for h
• Know I need U, so find hext
• For Forced External Convection:
NuD = .3 + (.62ReD
1/2Pr1/3)/(1+(.4/Pr)2/3)1/4 * (1+(ReD/282000)5/8)4/5
Re = uD/ ϒ
u = ufan = (rpm(rmax)+rpm(rmin)/2)cos θ
Pr = ϒ/α
α = kair/ ρairCpair
NuD = hextD/kf