bagofmilk
Aerospace
- Dec 14, 2013
- 3
First of all, what is the name of this equation:
ΔT = SPtotal / (2.7*ηf)
This is used in HVAC applications to determine the total temperature rise across the supply fan.
Where:
ΔT = change in temperature (F)
SP = Total Static Pressure (inH2O)
ηf = fan efficiency (decimal form)
And where is this derived from? Can someone provide a link or specifics?
I started off with the first law:
Assume:
m_dot(1) = m_dot(2) = m_dot
Δz = 0
ΔU = 0 = Q - W + m_dot(Δh + 0.5(ΔV2))
Δh = cpΔT
m_dot = ρAV
This seemed to get me nowhere...so I went to Bernoulli's (neglect altitude change)
(P1/ρ) + 0.5(V12) = (P2/ρ) + 0.5(V22)
ΔP = 0.5ρ(ΔV2)
but I see nowhere where temperature is involved...im lost.
ΔT = SPtotal / (2.7*ηf)
This is used in HVAC applications to determine the total temperature rise across the supply fan.
Where:
ΔT = change in temperature (F)
SP = Total Static Pressure (inH2O)
ηf = fan efficiency (decimal form)
And where is this derived from? Can someone provide a link or specifics?
I started off with the first law:
Assume:
m_dot(1) = m_dot(2) = m_dot
Δz = 0
ΔU = 0 = Q - W + m_dot(Δh + 0.5(ΔV2))
Δh = cpΔT
m_dot = ρAV
This seemed to get me nowhere...so I went to Bernoulli's (neglect altitude change)
(P1/ρ) + 0.5(V12) = (P2/ρ) + 0.5(V22)
ΔP = 0.5ρ(ΔV2)
but I see nowhere where temperature is involved...im lost.