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Turbomachinery Lecture 3 Compressibility Isentropic
Area, Mass Flow Functions C-D Nozzle
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Turbomachinery Definition:
A turbomachine transfers energy to or from a fluid moving continuously through a casing by dynamic action of a rotor and by flow conditioning of a stator. Works on a fluid to produce power or flow (and pressure rise) Adds energy to fluid Pump or Compressor Fan: pressure rise up to lbf/in2 Blower: pressure between lbf/in2 Compressor: pressure rise > 40 lbf/in2 Extracts energy from fluid Turbine Pressure changes due to motion of parts or displacement of boundaries
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Compressible Flow Density varies making continuity & momentum more difficult to solve. because varies with velocity. Also, can't integrate Bernoulli directly Compressible flow problems can be solved iteratively using continuity, state et. al. α C
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Compressible Flow Example: m = 50 lb/sec A = 200 sq.in.
P0 = 14.7 psia = 30 T0 = 519 R Guess C = ft/sec
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Compressible Flow Pressure
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Compressible Flow Density can now be found from state:
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Compressible Flow Mass Flow: note: 19%>
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Compressible Flow Mach Number Functions:
Easily calculated & clarify physics Mach number & acoustic speed are critical concepts!
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Compressible Flow
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Compressible Flow Using isentropic relation between pressure & temperature derivatives: Use adiabatic state law
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Compressible Flow Using equation of state, acoustic speed in an ideal gas is [from kinetic theory]: By definition Mach Number is:
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Compressible Flow Static & Total properties as functions of Mach number:
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Compressible Flow – Critical Velocity
What does subscript * mean? It means value of variable when M=1 [sonic] Vcr is only function of gas [] and stagnation props.
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Compressible Flow The relation between static & stagnation properties is isentropic. Then:
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Compressible Flow The relation between compressible and Bernoulli [B-p.55]
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Compressible Flow Relationships
Mass Flow parameter [=0]
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Compressible Flow Relationships
Area-Mach number differential relation Area-Mach number integral relation More on next chart
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Compressible Flow Relationships
What does subscript * mean? For all flow variables it means value of variable when M=1 [sonic] For area A* this is reference area for choking flow [M=1] Note this area is a minimum or throat More on next chart
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Compressible Flow Relationships
Compressible Aero Calculator calcbody2 Flow textbooks
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Compressible Flow Relations
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Of interest here Of interest here
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Over-expanded
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Compressible Flow Examples
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Compressible Flow Examples
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Compressible Flow Mass Flow Parameters:
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Compressible Flow Relationships
Mass flow parameters Note: FPo, FPs are similar, but different f[M] powers
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Compressible Flow Relationships
Mass flow parameters How to get more mass flow, i.e. greater thrust, more power?
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Compressible Flow Relationships
Mass flow parameters in English units m in lbm/sec p0A in lbf [spatial dimensions cancel] T0 in degs. Rankine
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Compressible Flow Relationships
Mass flow parameters in SI units m in kg/sec p0A in Newtons [spatial dimensions cancel] T0 in degs. Kelvin
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Compressible Flow Examples
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Example
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Static Pressure Mass Flow Parameter
Defining: FP = Flow parameter=f(M) For Air Can be inverted
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Total Pressure Mass Flow Parameter
Introducing P0: No explicit solution for M FPs is single valued, FPo is not FPo max = for =1.4 FPo max always at M=1
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Calculate FPo From Previous Example: m = 50 lb/sec A = 200 sq.in.
P0 = 14.7 psia = 30 T0 = 519 R Rearrange FPo
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Mass Flow Parameters Be careful: FPs single valued, FPo double values
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Total Pressure Mass Flow Parameter
Consider FPt: For fixed , a fixed value of produces the same Mach number - regardless of the level of pressure, temperature or molecular weight (R).
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Total Pressure Mass Flow Parameter
Defines common flow parameters. Valid for flow with one gas. Corrected flow.
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Other Parameters [Covered in Lecture 4]
Ideal gas equation for Mach number leads to speed parameters, also for a single gas. Speed parameter Corrected speed
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Significance of Flow & Speed Parameters
A device operating at: same speed parameter and flow parameter has same Mach numbers, velocity diagrams, flow angles etc, regardless of level of physical speed, pressure & temperature.
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Flow and Speed Parameters
Conditions: same gas, high Reynolds number, same clearances, and same Speed and Flow parameters are used for turbine maps
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Corrected Flow & Speed Parameters
Corrected Flow and Corrected speed used for compressor maps
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Flow Parameter Again, Consider FP0:
Unlike P, T & R; cannot be "corrected". Changing , changes relation between FP0 and Mach number!
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Flow Parameter Message: More complex gasses choke at a lower Mach number
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