∮ Thermodynamics熱力學
Chapters章節  /  03 Laws03 定律

Mass & Energy Analysis of Control Volumes控制體積的質量與能量分析

Most real equipment is an open system — mass flows through it. Add conservation of mass and the flow-work term to the first law and you get the steady-flow energy equation: the single relation behind nozzles, turbines, compressors, throttles, and heat exchangers.大多數實際裝置是開放系統——質量流透其中。將質量守恆與流動功項加入第一定律,就得到穩態流動能量方程式:噴嘴、渦輪機、壓縮機、節流閥與熱交換器背後的唯一關係式。

SFEE device explorer Which terms drop out
Overview總覽

What you'll be able to do本章學習成果

  • Apply conservation of mass to steady- and unsteady-flow control volumes.
  • Identify the energy a stream carries — internal, flow work, kinetic, potential — and fold the first two into enthalpy.
  • Solve steady-flow energy balances for nozzles, turbines, compressors, throttles, mixers, and heat exchangers.
  • Analyze unsteady (uniform-flow) charging and discharging processes.

Key equations重要公式

Mass rate balance質量速率平衡
$dm_{cv}/dt = \sum\dot m_i - \sum\dot m_e$
Steady-flow energy (1-in,1-out)穩態流動能量(1進1出)
$0 = \dot Q - \dot W + \dot m[(h_1-h_2)+\tfrac{\mathcal{V}_1^2-\mathcal{V}_2^2}{2}+g(z_1-z_2)]$
Turbine / throttle渦輪機 / 節流閥
$\dot W = \dot m(h_1-h_2)\;;\;\; h_2 = h_1$
Open systems開放系統

What is a control volume?什麼是控制體積?

Fluid flows continuously through a pipe, nozzle or turbine. Following one fixed lump of mass (a closed system) is awkward: it enters, passes through and leaves. Instead, fix a region in space and track everything that crosses its surface.流體持續流經管路、噴嘴或渦輪機。追蹤固定的一團質量(封閉系統)並不方便:它流入、通過、再流出。改為固定一個空間區域,追蹤所有穿越其表面的量。

ṁ1ṁ2Control volume (CV)控制體積(CV)a fixed region in space空間中固定的區域ẆcvQ̇cvControl surface (CS)控制面(CS)Inlet 1入口 1p1, T1, V1, A1Exit 2出口 2p2, T2, V2, A2Surroundings外界
A tube section as a control volume. The control surface (dashed) follows the real tube wall and cuts across the flow at two imaginary planes, inlet 1 and exit 2. Mass, heat and work can all cross it.以一段管路作為控制體積。控制面(虛線)沿實際管壁,並在入口 1 與出口 2 兩個假想截面橫切流動。質量、熱與功皆可穿越。
  • Control volume (CV): a region in space chosen for analysis. Mass, heat and work can all cross its boundary.控制體積(CV):選定分析的空間區域。質量、熱與功皆可穿越其邊界。
  • Control surface (CS): the boundary of the CV. Part of it can be real (the tube wall) and part imaginary (the inlet and exit planes).控制面(CS):CV 的邊界。可部分為實體(管壁)、部分為假想(入口與出口截面)。
  • Inlets $i$ and exits $e$: where mass crosses the CS. Here, inlet 1 and exit 2.入口 $i$ 與出口 $e$:質量穿越 CS 之處。此處為入口 1 與出口 2。
  • CV vs closed system: a closed system keeps the same mass; a CV keeps the same region, so different molecules occupy it at each instant.CV 與封閉系統:封閉系統保持相同質量;CV 保持相同區域,因此每一瞬間占據其中的分子不同。
  • One-dimensional flow: at each inlet and exit, properties ($p$, $T$, $v$, $\mathcal{V}$) are uniform over the area and the flow is normal to it. Assumed throughout this chapter.一維流動:每個入口與出口截面上,性質($p$、$T$、$v$、$\mathcal{V}$)均勻,且流動垂直於截面。本章全程採此假設。
Conservation守恆

Conservation of mass質量守恆

For a closed system, mass conservation is trivial: $m$ = constant. A CV can gain or lose mass through its ports. Take a general CV with several inlets and exits, and watch it over a short time $\Delta t$.對封閉系統,質量守恆不言自明:$m$ 為常數。CV 則可經由開口增減質量。取一具多個入口與出口的一般 CV,觀察一段短時間 $\Delta t$。

Δm1Δm2Δm3Δm4Δm5ṁ1ṁ2ṁ3ṁ4ṁ5mcvmass inside內部質量During a short time Δt: in Δm1 + Δm2, out Δm3 + Δm4 + Δm5短時間 Δt 內:流入 Δm1 + Δm2,流出 Δm3 + Δm4 + Δm5
A control volume with two inlets and three exits. During $\Delta t$ the shaded slugs cross the control surface: those at inlets 1–2 enter, those at exits 3–5 leave.具兩個入口與三個出口的控制體積。在 $\Delta t$ 內,著色的流體塊穿越控制面:入口 1–2 者流入,出口 3–5 者流出。

Step 1 — Bookkeeping over $\Delta t$步驟 1 — $\Delta t$ 內的記帳

Mass is neither created nor destroyed, so the change of mass inside equals what came in minus what went out:質量不生不滅,因此內部質量的變化等於流入減流出:

$$ m_{cv}(t+\Delta t) - m_{cv}(t) = \sum_i \Delta m_i - \sum_e \Delta m_e $$

Step 2 — Rate form步驟 2 — 速率形式

Divide by $\Delta t$ and let $\Delta t \to 0$. Each $\Delta m/\Delta t$ becomes a mass flow rate $\dot m$ (kg/s):除以 $\Delta t$ 並令 $\Delta t \to 0$。每個 $\Delta m/\Delta t$ 成為質量流率 $\dot m$(kg/s):

$$ \underbrace{\frac{dm_{cv}}{dt}}_{\text{rate of change inside}} = \underbrace{\sum_i \dot m_i}_{\text{total in}} - \underbrace{\sum_e \dot m_e}_{\text{total out}} $$
Eq. 4.2

For the figure, with two inlets and three exits:以圖為例,兩個入口、三個出口:

$$ \frac{dm_{cv}}{dt} = (\dot m_1 + \dot m_2) - (\dot m_3 + \dot m_4 + \dot m_5) $$

Step 3 — Mass flow rate at a port步驟 3 — 開口處的質量流率

In $\Delta t$ the slug at a port fills a cylinder of area $A$ and length $\mathcal{V}\Delta t$ (see the flow-work figure below). Its volume is在 $\Delta t$ 內,開口處的流體塊填滿截面積 $A$、長度 $\mathcal{V}\Delta t$ 的柱體(見下方流動功圖)。其體積為

$$ \Delta V = A\,\mathcal{V}\,\Delta t $$

Multiply by the density to get its mass:乘以密度得其質量:

$$ \Delta m = \rho\,\Delta V = \rho A \mathcal{V}\,\Delta t $$

Divide by $\Delta t$ and use $\rho = 1/v$:除以 $\Delta t$,並利用 $\rho = 1/v$:

$$ \dot m = \rho A \mathcal{V} = \frac{A\mathcal{V}}{v} $$
Mass flow rate

Step 4 — Steady state步驟 4 — 穩態

Steady state: nothing inside the CV changes with time, so the left side of Eq. 4.2 is zero:穩態:CV 內部不隨時間變化,故式 4.2 左側為零:

$$ \frac{dm_{cv}}{dt} = 0 \quad\Longrightarrow\quad \sum_i \dot m_i = \sum_e \dot m_e $$

For the figure:以圖為例:

$$ \dot m_1 + \dot m_2 = \dot m_3 + \dot m_4 + \dot m_5 $$

One inlet, one exit: substitute $\dot m = \rho A \mathcal{V}$ on each side:單一入口、單一出口:兩側代入 $\dot m = \rho A \mathcal{V}$:

$$ \dot m_1 = \dot m_2 \quad\Longrightarrow\quad \rho_1 A_1 \mathcal{V}_1 = \rho_2 A_2 \mathcal{V}_2 $$

Incompressible ($\rho_1 = \rho_2$): the density cancels, so the volume flow rate is conserved too:不可壓縮($\rho_1 = \rho_2$):密度相消,體積流率亦守恆:

$$ A_1 \mathcal{V}_1 = A_2 \mathcal{V}_2 $$
A key idea核心概念

Flow work & enthalpy流動功與焓

Mass entering a CV must be pushed in against the pressure of the fluid already there. The fluid behind does the pushing, and that work is flow work. Return to the one-inlet, one-exit tube.流入 CV 的質量必須克服其中流體的壓力被推入。由後方流體推動,此功即為流動功。回到單一入口、單一出口的管路。

Δm1Δm2p1A1p2A2V1ΔtV2Δtfluid behind後方流體CVCVpushed IN: work done on the CV推入:對 CV 做功p1A1·V1Δt = p1v1Δm1pushed OUT: work done by the CV推出:CV 對外做功p2A2·V2Δt = p2v2Δm2
Flow work. At inlet 1 the fluid behind pushes the slug $\Delta m_1$ (length $\mathcal{V}_1\Delta t$) into the CV with force $p_1A_1$. At exit 2 the CV pushes $\Delta m_2$ out against $p_2A_2$.流動功。在入口 1,後方流體以力 $p_1A_1$ 將流體塊 $\Delta m_1$(長度 $\mathcal{V}_1\Delta t$)推入 CV;在出口 2,CV 克服 $p_2A_2$ 將 $\Delta m_2$ 推出。

Step 1 — Work to push one slug in步驟 1 — 推入一個流體塊所需的功

The fluid behind the slug at inlet 1 pushes with force $F = p_1A_1$ through a distance $\mathcal{V}_1\Delta t$:入口 1 處流體塊後方的流體以力 $F = p_1A_1$ 推動,距離為 $\mathcal{V}_1\Delta t$:

$$ W_{flow,1} = F\,\Delta x = (p_1A_1)(\mathcal{V}_1\Delta t) $$

Step 2 — Per unit mass步驟 2 — 換成單位質量

The product $A_1\mathcal{V}_1\Delta t$ is the slug's volume, which is also its mass times its specific volume:$A_1\mathcal{V}_1\Delta t$ 即流體塊體積,亦等於其質量乘以比容:

$$ A_1\mathcal{V}_1\Delta t = v_1\,\Delta m_1 $$

Substitute into Step 1, then divide by $\Delta t$:代入步驟 1,再除以 $\Delta t$:

$$ W_{flow,1} = p_1 v_1\,\Delta m_1 \quad\xrightarrow{\;\div\,\Delta t\;}\quad \dot W_{flow,1} = \dot m_1\,p_1 v_1 $$
Flow work
  • At an inlet, work is done on the CV: energy in.入口處,功對 CV 做:能量流入。
  • At an exit, the CV pushes the fluid ahead of it: work done by the CV, $\dot m_2\,p_2v_2$, energy out.出口處,CV 推動前方流體:由 CV 做功 $\dot m_2\,p_2v_2$,能量流出。
  • Flow work exists only where mass crosses the CS; none acts at the solid walls.流動功只存在於質量穿越 CS 之處;固體壁面上沒有流動功。

Net flow work done by the CV (exit minus inlet):CV 所做淨流動功(出口減入口):

$$ \dot W_{flow} = \dot m_2\,p_2v_2 - \dot m_1\,p_1v_1 $$

Step 3 — Bundle with internal energy: enthalpy步驟 3 — 與內能合併:焓

Every kilogram crossing a port brings its internal energy $u$ and its flow work $pv$ together. The sum is a property we already know:每公斤穿越開口的質量同時帶著內能 $u$ 與流動功 $pv$。兩者之和是已知的性質:

$$ u + pv = h \quad(\text{enthalpy}) $$
Flow energy
Why enthalpy shows up everywhere為何焓到處出現

For any flowing stream, $h$ automatically includes both the internal energy and the flow work needed to move it. That is why control-volume balances are written in $h$, not $u$.對任何流動的流體,$h$ 自動包含內能與推動它所需的流動功。這就是控制體積平衡式以 $h$ 而非 $u$ 表示的原因。

The balance平衡式

Control-volume energy rate balance控制體積能量速率平衡

Follow the same logic as the closed system: energy conservation for a region, now with mass also carrying energy across the boundary. Take one inlet $i$ and one exit $e$ first.沿用封閉系統的邏輯:對一區域做能量守恆,如今質量也攜帶能量穿越邊界。先取單一入口 $i$ 與單一出口 $e$。

Ecv(t)energy stored儲存能量ẆcvQ̇cvṁi ( ui + pivi + Vi2/2 + gzi )ṁe ( ue + peve + Ve2/2 + gze )inlet i入口 iexit e出口 edatum z = 0基準面 z = 0zize
Energy accounting. Besides heat and shaft work, each kilogram crossing the control surface carries $u + \mathcal{V}^2/2 + gz$ and brings its own flow work $pv$ (green term).能量帳目。除熱與軸功外,每公斤穿越控制面的質量攜帶 $u + \mathcal{V}^2/2 + gz$,並附帶其流動功 $pv$(綠色項)。

Step 1 — Conservation over $\Delta t$步驟 1 — $\Delta t$ 內的守恆

$$ \underbrace{E_{cv}(t+\Delta t) - E_{cv}(t)}_{\text{change of energy stored}} = \underbrace{E_{in} - E_{out}}_{\text{net energy transferred across CS}} $$

This is the closed-system statement. Only the list of ways in and out grows.這與封閉系統的敘述相同,只是能量進出的方式變多了。

Step 2 — List every transfer步驟 2 — 列出所有傳遞方式

  • Heat $Q$: as before, $Q > 0$ into the CV.熱 $Q$:同前,$Q > 0$ 為進入 CV。
  • Work $W$: all work, $W > 0$ done by the CV. It splits into flow work at the ports and everything else, $W_{cv}$ (shaft, electrical, moving boundary).功 $W$:所有的功,$W > 0$ 為 CV 對外做功。可分為開口處的流動功,與其餘所有功 $W_{cv}$(軸功、電功、移動邊界功)。
  • Mass: each kilogram crossing carries its stored energy (internal + kinetic + potential):質量:每公斤穿越的質量攜帶其儲存能量(內能 + 動能 + 位能):
$$ e = u + \frac{\mathcal{V}^2}{2} + gz $$

Step 3 — Finite form over $\Delta t$步驟 3 — $\Delta t$ 內的有限形式

$$ E_{cv}(t+\Delta t) - E_{cv}(t) = Q - W + \Delta m_i\left(u_i + \tfrac{\mathcal{V}_i^2}{2} + gz_i\right) - \Delta m_e\left(u_e + \tfrac{\mathcal{V}_e^2}{2} + gz_e\right) $$

Step 4 — Rate form步驟 4 — 速率形式

Divide by $\Delta t$ and let $\Delta t \to 0$:除以 $\Delta t$ 並令 $\Delta t \to 0$:

$$ \frac{dE_{cv}}{dt} = \dot Q - \dot W + \dot m_i\left(u_i + \tfrac{\mathcal{V}_i^2}{2} + gz_i\right) - \dot m_e\left(u_e + \tfrac{\mathcal{V}_e^2}{2} + gz_e\right) $$

Step 5 — Separate the flow work步驟 5 — 分離流動功

From the previous section, the total work rate is the useful work plus the net flow work:由前一節,總功率為有用功加上淨流動功:

$$ \dot W = \dot W_{cv} + \dot m_e\,p_e v_e - \dot m_i\,p_i v_i $$

Substitute. Each $pv$ term joins the $u$ of its own stream:代入後,各 $pv$ 項併入其流體的 $u$:

$$ \frac{dE_{cv}}{dt} = \dot Q_{cv} - \dot W_{cv} + \dot m_i\left(u_i + p_iv_i + \tfrac{\mathcal{V}_i^2}{2} + gz_i\right) - \dot m_e\left(u_e + p_ev_e + \tfrac{\mathcal{V}_e^2}{2} + gz_e\right) $$

Step 6 — Enthalpy and many ports步驟 6 — 焓與多個開口

Replace $u + pv$ with $h$ and sum over all inlets and exits:以 $h$ 取代 $u + pv$,並對所有入口與出口加總:

$$ \frac{dE_{cv}}{dt} = \dot Q_{cv} - \dot W_{cv} + \sum_i \dot m_i\!\left(h_i + \tfrac{\mathcal{V}_i^2}{2} + gz_i\right) - \sum_e \dot m_e\!\left(h_e + \tfrac{\mathcal{V}_e^2}{2} + gz_e\right) $$
Eq. 4.15
  • $\dot W_{cv}$ excludes flow work; it is already inside $h$.$\dot W_{cv}$ 不含流動功,流動功已包含在 $h$ 中。

Check: close every port ($\dot m_i = \dot m_e = 0$). The sums vanish and the closed-system rate form returns:驗證:關閉所有開口($\dot m_i = \dot m_e = 0$),加總項消失,回到封閉系統的速率形式:

$$ \frac{dE}{dt} = \dot Q - \dot W $$
Workhorse主要工具

Steady-flow form (SFEE)穩態流動形式(SFEE)

Step 1 — Steady state. Nothing inside the CV changes with time:步驟 1 — 穩態。CV 內部不隨時間變化:

$$ \frac{dm_{cv}}{dt} = 0, \qquad \frac{dE_{cv}}{dt} = 0 $$

Step 2 — One inlet, one exit. The mass balance gives步驟 2 — 單一入口、單一出口。質量平衡得

$$ \dot m_1 = \dot m_2 = \dot m $$

Step 3 — Substitute into Eq. 4.15 and factor out $\dot m$:步驟 3 — 代入式 4.15,並提出 $\dot m$:

$$ 0 = \dot Q_{cv} - \dot W_{cv} + \dot m\left[(h_1 - h_2) + \frac{\mathcal{V}_1^2 - \mathcal{V}_2^2}{2} + g(z_1 - z_2)\right] $$

Step 4 — Per unit mass. Divide by $\dot m$ to get the steady-flow energy equation:步驟 4 — 單位質量。除以 $\dot m$,得穩態流動能量方程式:

$$ 0 = \frac{\dot Q_{cv}}{\dot m} - \frac{\dot W_{cv}}{\dot m} + (h_1 - h_2) + \frac{\mathcal{V}_1^2 - \mathcal{V}_2^2}{2} + g(z_1 - z_2) $$
Eq. 4.20b
  • Units: $\mathcal{V}^2/2$ and $gz$ come out in J/kg; divide by 1000 to match $h$ in kJ/kg. For example, $\mathcal{V} = 100$ m/s gives $\mathcal{V}^2/2 = 5000$ J/kg $= 5$ kJ/kg.單位:$\mathcal{V}^2/2$ 與 $gz$ 的單位為 J/kg;除以 1000 才與 kJ/kg 的 $h$ 一致。例如 $\mathcal{V} = 100$ m/s,$\mathcal{V}^2/2 = 5000$ J/kg $= 5$ kJ/kg。
  • Analyzing any device is then a matter of deciding which terms are negligible.分析任何裝置,便只需判斷哪些項可忽略。
Applying the balance平衡式應用

From the balance to real equipment從平衡式到實際裝置

Eq. 4.20b has five terms: heat $q$, work $w$, enthalpy change $\Delta h$, kinetic-energy change $\Delta\mathcal{V}^2/2$ and potential-energy change $g\Delta z$. A real device rarely needs all five. Before writing any numbers, go through the terms one at a time and decide whether each one matters for that device.式 4.20b 共有五項:熱 $q$、功 $w$、焓變化 $\Delta h$、動能變化 $\Delta\mathcal{V}^2/2$ 與位能變化 $g\Delta z$。實際裝置很少需要全部五項。代入數字前,應逐項檢查,判斷每一項對該裝置是否重要。

Term項Usually dropped when…通常可忽略的情況Kept when…需保留的情況
$\dot Q_{cv}$the device is insulated, or the flow passes through too fast to exchange much heat裝置有隔熱,或流體通過太快、來不及大量換熱heating or cooling is the purpose (boiler, condenser) or the casing is deliberately cooled加熱或冷卻即為目的(鍋爐、冷凝器),或外殼刻意冷卻
$\dot W_{cv}$there is no shaft or electrical input, only a duct or valve沒有軸或電力輸入,僅為管道或閥門a rotating shaft crosses the boundary (turbine, pump, compressor)有轉軸穿越邊界(渦輪機、泵、壓縮機)
$\Delta\mathcal{V}^2/2$inlet and exit speeds are similar or low (below about 50 m/s, i.e. under about 1 kJ/kg)進出口速度相近或偏低(約 50 m/s 以下,即約 1 kJ/kg 以下)changing the speed is the purpose (nozzle, diffuser)改變流速即為目的(噴嘴、擴散器)
$g\Delta z$almost always: a 10 m rise is only 0.1 kJ/kg幾乎總是可忽略:上升 10 m 僅 0.1 kJ/kglarge height changes with small other terms (hydro plants, tall pumping lines)高度變化大而其他項小(水力電廠、高揚程管線)

Whatever survives is the working equation for that device. For example, an insulated turbine keeps $\dot W$ and $\Delta h$; an insulated nozzle keeps $\Delta h$ and the kinetic term; a valve drops every term except $\Delta h$, which must then be zero, so $h_2 = h_1$. The next chapter, Steady-Flow Devices, applies this checklist to seven common devices one by one, with applications and typical efficiencies. The interactive SFEE device explorer is in Flow Devices & Isentropic Efficiency.剩下的項即為該裝置的工作方程式。例如:隔熱渦輪機保留 $\dot W$ 與 $\Delta h$;隔熱噴嘴保留 $\Delta h$ 與動能項;閥門除 $\Delta h$ 外各項皆可忽略,故 $\Delta h = 0$,即 $h_2 = h_1$。下一章 穩態流動裝置 將以此檢查表逐一分析七種常見裝置,並介紹其應用與典型效率。互動式 SFEE 裝置探索器請見 流動裝置與等熵效率。

Beyond steady超越穩態

Unsteady (uniform-flow) processes非穩態(均勻流動)過程

Charging or discharging a tank changes the inventory with time. Integrating the rate balances over the process gives the mass and energy accounting:

$$ m_{cv}(t) - m_{cv}(0) = \sum m_i - \sum m_e $$
Eq. 4.23

In the uniform-flow model, inlet and exit properties are taken constant, so $U_{cv}(t) - U_{cv}(0) = Q_{cv} - W_{cv} + \sum m_i h_i - \sum m_e h_e$. With all ports closed, this collapses back to the closed-system energy balance — the two views are consistent.

Try it — filling a tank動手試試——儲罐充氣

Charge a rigid, insulated tank from a high-pressure supply line. The uniform-flow energy balance gives a striking result: the gas already in the tank does compression work on the incoming gas, so the final temperature ends up above the line temperature. Fill an evacuated tank and $T_2 = k\,T_{line}$ — about 40% hotter for air.

Rigid adiabatic tank, air as ideal gas. Filled until tank pressure reaches the supply-line pressure.

Worked example範例

Applying the control-volume energy balance控制體積能量平衡的應用

Example 1範例 1 Air compressor with heat loss有熱損失的空氣壓縮機 ›

Given: air enters a compressor at $p_1 = 100$ kPa, $T_1 = 300$ K, $\mathcal{V}_1 = 6$ m/s through an inlet area $A_1 = 0.1$ m². It leaves at $p_2 = 400$ kPa, $T_2 = 460$ K, $\mathcal{V}_2 = 30$ m/s. The compressor loses 10 kW of heat to the surroundings. Steady state; ideal gas, $R = 0.287$, $c_p = 1.005$ kJ/kg·K; $\Delta z = 0$.已知:空氣以 $p_1 = 100$ kPa、$T_1 = 300$ K、$\mathcal{V}_1 = 6$ m/s 經入口面積 $A_1 = 0.1$ m² 流入壓縮機,以 $p_2 = 400$ kPa、$T_2 = 460$ K、$\mathcal{V}_2 = 30$ m/s 流出。壓縮機向外界散熱 10 kW。穩態;理想氣體,$R = 0.287$、$c_p = 1.005$ kJ/kg·K;$\Delta z = 0$。

Find: the mass flow rate $\dot m$, the power input $\dot W_{cv}$, and the exit area $A_2$.求:質量流率 $\dot m$、輸入功率 $\dot W_{cv}$ 與出口面積 $A_2$。

Step 1 — Define the control volume. Draw the CS around the compressor casing, cutting the inlet pipe at 1 and the exit pipe at 2. Mass crosses at 1 and 2, so this is a control volume with one inlet and one exit. Heat crosses the casing; shaft work crosses where the drive shaft enters.步驟 1 — 定義控制體積。沿壓縮機外殼畫出 CS,並在入口管 1 與出口管 2 處切開。質量於 1 與 2 穿越,因此為單一入口、單一出口的控制體積。熱穿越外殼;軸功由驅動軸穿越。

Step 2 — Mass balance. Steady state: $dm_{cv}/dt = 0$, so $\dot m_1 = \dot m_2 = \dot m$. Get $\dot m$ from the inlet, where $A$ and $\mathcal{V}$ are known. First the specific volume from the ideal-gas law: $$v_1 = \frac{RT_1}{p_1} = \frac{(0.287)(300)}{100} = 0.861\ \text{m}^3/\text{kg}$$ Then $$\dot m = \frac{A_1\mathcal{V}_1}{v_1} = \frac{(0.1)(6)}{0.861} = 0.697\ \text{kg/s}$$步驟 2 — 質量平衡。穩態:$dm_{cv}/dt = 0$,故 $\dot m_1 = \dot m_2 = \dot m$。由已知 $A$ 與 $\mathcal{V}$ 的入口求 $\dot m$。先由理想氣體定律求比容:$$v_1 = \frac{RT_1}{p_1} = \frac{(0.287)(300)}{100} = 0.861\ \text{m}^3/\text{kg}$$ 再得 $$\dot m = \frac{A_1\mathcal{V}_1}{v_1} = \frac{(0.1)(6)}{0.861} = 0.697\ \text{kg/s}$$

Step 3 — Write the general energy rate balance. $$\frac{dE_{cv}}{dt} = \dot Q_{cv} - \dot W_{cv} + \dot m\left[(h_1 - h_2) + \frac{\mathcal{V}_1^2 - \mathcal{V}_2^2}{2} + g(z_1 - z_2)\right]$$步驟 3 — 寫出一般能量速率平衡式。 $$\frac{dE_{cv}}{dt} = \dot Q_{cv} - \dot W_{cv} + \dot m\left[(h_1 - h_2) + \frac{\mathcal{V}_1^2 - \mathcal{V}_2^2}{2} + g(z_1 - z_2)\right]$$

Step 4 — Simplify term by term.
• Steady state: $dE_{cv}/dt = 0$.
• $\Delta z = 0$: the potential-energy term drops.
• Heat leaves, so with $Q > 0$ meaning in, $\dot Q_{cv} = -10$ kW.
• Keep the kinetic-energy term for now and check its size.
Solving for the work: $$\dot W_{cv} = \dot Q_{cv} + \dot m\left[(h_1 - h_2) + \frac{\mathcal{V}_1^2 - \mathcal{V}_2^2}{2}\right]$$
步驟 4 — 逐項化簡。
• 穩態:$dE_{cv}/dt = 0$。
• $\Delta z = 0$:位能項消去。
• 熱流出,而 $Q > 0$ 表示流入,故 $\dot Q_{cv} = -10$ kW。
• 暫保留動能項,再檢查其大小。
解出功:$$\dot W_{cv} = \dot Q_{cv} + \dot m\left[(h_1 - h_2) + \frac{\mathcal{V}_1^2 - \mathcal{V}_2^2}{2}\right]$$

Step 5 — Evaluate each term per unit mass.
• Enthalpy (ideal gas, constant $c_p$): $$h_1 - h_2 = c_p(T_1 - T_2) = (1.005)(300 - 460) = -160.8\ \text{kJ/kg}$$ • Kinetic energy, converting J/kg to kJ/kg: $$\frac{\mathcal{V}_1^2 - \mathcal{V}_2^2}{2} = \frac{6^2 - 30^2}{2} = -432\ \text{J/kg} = -0.432\ \text{kJ/kg}$$ The KE term is under 0.3% of the enthalpy term, so it is negligible here.
步驟 5 — 逐項計算(單位質量)。
• 焓(理想氣體、常 $c_p$):$$h_1 - h_2 = c_p(T_1 - T_2) = (1.005)(300 - 460) = -160.8\ \text{kJ/kg}$$ • 動能,由 J/kg 換成 kJ/kg:$$\frac{\mathcal{V}_1^2 - \mathcal{V}_2^2}{2} = \frac{6^2 - 30^2}{2} = -432\ \text{J/kg} = -0.432\ \text{kJ/kg}$$ 動能項不到焓項的 0.3%,此處可忽略。

Step 6 — Solve for the power. $$\dot W_{cv} = -10 + (0.697)(-160.8 - 0.432) = -10 - 112.4 = -122.4\ \text{kW}$$步驟 6 — 求功率。 $$\dot W_{cv} = -10 + (0.697)(-160.8 - 0.432) = -10 - 112.4 = -122.4\ \text{kW}$$

Step 7 — Exit area from the mass balance. $$v_2 = \frac{RT_2}{p_2} = \frac{(0.287)(460)}{400} = 0.330\ \text{m}^3/\text{kg}, \qquad A_2 = \frac{\dot m\,v_2}{\mathcal{V}_2} = \frac{(0.697)(0.330)}{30} = 0.0077\ \text{m}^2$$步驟 7 — 由質量平衡求出口面積。 $$v_2 = \frac{RT_2}{p_2} = \frac{(0.287)(460)}{400} = 0.330\ \text{m}^3/\text{kg}, \qquad A_2 = \frac{\dot m\,v_2}{\mathcal{V}_2} = \frac{(0.697)(0.330)}{30} = 0.0077\ \text{m}^2$$

Step 8 — Check. $\dot W_{cv} < 0$: work is done on the air, as expected for a compressor. The heat loss adds to the required power: the motor must supply both the enthalpy rise and the 10 kW lost. Units: kg/s × kJ/kg = kW ✓.步驟 8 — 檢驗。$\dot W_{cv} < 0$:外界對空氣做功,符合壓縮機的預期。熱損失使所需功率增加:馬達須同時供應焓的增加與散失的 10 kW。單位:kg/s × kJ/kg = kW ✓。

Answer: $\dot m = 0.697$ kg/s, $\dot W_{cv} \approx -122$ kW (122 kW input), $A_2 \approx 0.0077$ m².答:$\dot m = 0.697$ kg/s,$\dot W_{cv} \approx -122$ kW(輸入 122 kW),$A_2 \approx 0.0077$ m²。

Example 2範例 2 Exit velocity from a nozzle噴嘴出口速度 ›

Given: air enters an adiabatic nozzle at $T_1 = 420$ K with $\mathcal{V}_1 = 10$ m/s and exits at $T_2 = 300$ K. Ideal gas, $c_p=1.005$ kJ/kg·K.已知:空氣以 $T_1 = 420$ K、$\mathcal{V}_1 = 10$ m/s 進入絕熱噴嘴,以 $T_2 = 300$ K 流出。理想氣體,$c_p=1.005$ kJ/kg·K。

Find: the exit velocity $\mathcal{V}_2$.求:出口速度 $\mathcal{V}_2$。

Step 1 — Start from the full energy rate balance (Eq. 4.15) with one inlet (1) and one exit (2): $$\frac{dE_{cv}}{dt} = \dot Q_{cv} - \dot W_{cv} + \dot m_1\!\left(h_1 + \tfrac{\mathcal{V}_1^2}{2} + gz_1\right) - \dot m_2\!\left(h_2 + \tfrac{\mathcal{V}_2^2}{2} + gz_2\right)$$步驟 1 — 由完整的能量速率平衡出發(式 4.15),單一入口 (1)、單一出口 (2):$$\frac{dE_{cv}}{dt} = \dot Q_{cv} - \dot W_{cv} + \dot m_1\!\left(h_1 + \tfrac{\mathcal{V}_1^2}{2} + gz_1\right) - \dot m_2\!\left(h_2 + \tfrac{\mathcal{V}_2^2}{2} + gz_2\right)$$

Step 2 — Steady state. Nothing inside the nozzle changes with time, so $dE_{cv}/dt = 0$, and the mass balance gives $\dot m_1 = \dot m_2 = \dot m$: $$0 = \dot Q_{cv} - \dot W_{cv} + \dot m\left[(h_1 - h_2) + \frac{\mathcal{V}_1^2 - \mathcal{V}_2^2}{2} + g(z_1 - z_2)\right]$$步驟 2 — 穩態。噴嘴內部不隨時間變化,故 $dE_{cv}/dt = 0$;質量平衡得 $\dot m_1 = \dot m_2 = \dot m$:$$0 = \dot Q_{cv} - \dot W_{cv} + \dot m\left[(h_1 - h_2) + \frac{\mathcal{V}_1^2 - \mathcal{V}_2^2}{2} + g(z_1 - z_2)\right]$$

Step 3 — Drop the negligible terms. Adiabatic: $\dot Q_{cv} = 0$. No shaft: $\dot W_{cv} = 0$. A nozzle is short and horizontal: $g(z_1 - z_2) \approx 0$. Divide by $\dot m$: $$0 = (h_1 - h_2) + \frac{\mathcal{V}_1^2 - \mathcal{V}_2^2}{2} \quad\Longrightarrow\quad h_1 - h_2 = \frac{\mathcal{V}_2^2 - \mathcal{V}_1^2}{2}$$ The enthalpy drop becomes kinetic energy.步驟 3 — 刪去可忽略的項。絕熱:$\dot Q_{cv} = 0$。無轉軸:$\dot W_{cv} = 0$。噴嘴短且水平:$g(z_1 - z_2) \approx 0$。除以 $\dot m$:$$0 = (h_1 - h_2) + \frac{\mathcal{V}_1^2 - \mathcal{V}_2^2}{2} \quad\Longrightarrow\quad h_1 - h_2 = \frac{\mathcal{V}_2^2 - \mathcal{V}_1^2}{2}$$ 焓的減少轉為動能。

Step 4 — Ideal-gas enthalpy. With constant $c_p$: $$h_1 - h_2 = c_p(T_1 - T_2) = 1.005(420 - 300) = 120.6\ \text{kJ/kg} = 120\,600\ \text{J/kg}$$ Convert to J/kg so the units match $\mathcal{V}^2/2$ (m²/s² = J/kg).步驟 4 — 理想氣體的焓。$c_p$ 為常數:$$h_1 - h_2 = c_p(T_1 - T_2) = 1.005(420 - 300) = 120.6\ \text{kJ/kg} = 120\,600\ \text{J/kg}$$ 換算為 J/kg,使單位與 $\mathcal{V}^2/2$(m²/s² = J/kg)一致。

Step 5 — Solve for the exit velocity. $$\mathcal{V}_2 = \sqrt{\mathcal{V}_1^2 + 2(h_1 - h_2)} = \sqrt{10^2 + 2(120\,600)} = 491\ \text{m/s}$$ The inlet term contributes only 100 m²/s² out of 241 300, which is why inlet velocity is often neglected in nozzles.步驟 5 — 求出口速度。$$\mathcal{V}_2 = \sqrt{\mathcal{V}_1^2 + 2(h_1 - h_2)} = \sqrt{10^2 + 2(120\,600)} = 491\ \text{m/s}$$ 入口項僅佔 241 300 中的 100 m²/s²,因此噴嘴分析常忽略入口速度。

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