Chemical Engineering 374 - BYU College of Engineeringmjm82/che374/Fall2016/...Chemical Engineering...

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1 Chemical Engineering 374 Fluid Mechanics Compressible Flow

Transcript of Chemical Engineering 374 - BYU College of Engineeringmjm82/che374/Fall2016/...Chemical Engineering...

Page 1: Chemical Engineering 374 - BYU College of Engineeringmjm82/che374/Fall2016/...Chemical Engineering 374 Fluid Mechanics Compressible Flow. Spiritual Thought 2 John 11:35 Jesus wept.

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Chemical Engineering 374

Fluid Mechanics

Compressible Flow

Page 2: Chemical Engineering 374 - BYU College of Engineeringmjm82/che374/Fall2016/...Chemical Engineering 374 Fluid Mechanics Compressible Flow. Spiritual Thought 2 John 11:35 Jesus wept.

Spiritual Thought2

John 11:35

Jesus wept.

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Fluids Roadmap

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Key Points

• Characteristics

– Converts u to kinetic energy

– T drops, ρ drops

– v greater than in non-compressible flow

– M

• Equations

• Nozzles

• Choked Flow

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Page 5: Chemical Engineering 374 - BYU College of Engineeringmjm82/che374/Fall2016/...Chemical Engineering 374 Fluid Mechanics Compressible Flow. Spiritual Thought 2 John 11:35 Jesus wept.

Compressible Flows

• Previously, ρ was constant

• Now, ρ varies

– High speed flow, large ΔP, ΔT, Δv, etc.

– Internal energy is converted to kinetic energy

• T Drops; ρ drops

• v > v of Bernoulli Eqn. where ρ is constant

– Mach number, M = v/c; c is local value, [c(T)]

– Compressible for M > 0.3, ρ/ρ ~ 0.95,

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Sound Speed6

P

ρ

v

P+dP

Ρ+dρ

V+dv

c

• Pressure Pulse Analysis

• Mass Balance

• Momentum Balance

• Expression for c

• Error

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• Mass Balance

• Momentum Balance

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• Sound waves compress

– No heat transfer

– Isentropic

– NOT isothermal

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𝑘 = ൘𝐶𝑝

𝐶𝑣= 1.4 𝑓𝑜𝑟 𝑎𝑖𝑟

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Common Values of c

c (m/s) c (mph)

Air @ 298 K 346 774

Air @ 2000 K 896 2000

H2O @ 288 K 1490 3333

Steel @ 188 K 5060 11318

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Page 10: Chemical Engineering 374 - BYU College of Engineeringmjm82/che374/Fall2016/...Chemical Engineering 374 Fluid Mechanics Compressible Flow. Spiritual Thought 2 John 11:35 Jesus wept.

Compressible Flow10

• Flow from Large Reservoir

• Stagnation condition

• Convenient reference

• Assume SS, 1-D, Ideal

Gas, no friction, ignore g

R

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• Energy Balance

• ሶ𝑄 + ሶ𝑊𝑠 = ሶ𝑚𝑃

𝜌+ 𝑢 +

𝑣2

2+ 𝑔𝑧

𝑅- ሶ𝑚

𝑃

𝜌+ 𝑢 +

𝑣2

2+ 𝑔𝑧

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• 𝑣1 = 2 ℎ𝑟 − ℎ1 = 2𝐶𝑝 𝑇𝑟 − 𝑇1

• Given: 𝐶𝑝 = 𝐶𝑣 +𝑅

𝑀𝑘 = ൗ

𝐶𝑝𝐶𝑣→ 𝐶𝑣 = ൗ𝐶𝑝

𝑘

• 𝐶𝑝 =𝑅𝑘

𝑀 𝑘−1

• 𝑐2 =𝑘𝑅𝑇

𝑀

•𝑣12

𝑐12 = 𝑀2 =

2

𝑘−1

𝑇𝑟

𝑇1− 1

•𝑇𝑟

𝑇1=

𝑀2 𝑘−1

2+ 1

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• Ideal Gases: (thermo, next semester…)

;

• Thus,

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Nozzles

• Mass flow = constant

• As A decreases, v increases

• Eventually v = c at (*)

– A1ρ1v1 = A*ρ*v*

– A1 / A* = ρ*v* / ρ1v1

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*

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• For M<1, as velocity increases, A

decreases

• For M > 1, as velocity increases, A

increases!

– Because ρ is decreasing faster than A is

increasing v increase to keep ሶ𝑚 = 𝜌𝐴𝑣constant

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Choked Flow

• Flow Changes “communicated” at speed of sound

• i.e. pressure waves – travel at c

• If flow speed increases to c, then communication wave

can’t get back to reservoir

– Shouting in wind

– “Communication” doesn’t occur

• Flow doesn’t increase not matter how low P2 becomes

– Choked flow

– Gas Control valves, orifices, vacuum systems, bike tires

– Choke point is minimum area in the nozzle/valve

• Flow is constant until ΔP decreases below Critical

pressure

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