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Chapter 1Introduction and Basic Con
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4-2 Energy Balance for Closed Syste
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7-2 The Increase of Entropy Princip
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Development of Gas TurbinesDeviatio
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ProblemsChapter 13Gas Mixtures13-1
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17-1 Stagnation Properties17-2 Spee
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Appendix 2Property Tables and Chart
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PREFACEBACKGROUNDThermodynamics is
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Preface | xixcoverage of oblique sh
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starts with the simplest case and a
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A CHOICE OF SI ALONE OR SI/ENGLISH
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Chapter 1INTRODUCTION AND BASIC CON
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particles to determine the pressure
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did not find universal acceptance u
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1 J 1 N # m (1-3)Chapter 1 | 7wher
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mN kgs 2andlbf 32.174 ftlbm s 2 C
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devices is best studied by selectin
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diameter) is much larger than the m
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A system is called a simple compres
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time in a periodic manner, and the
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points on a plane, these two measur
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We emphasize that the magnitudes of
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Chapter 1 | 23P gageP vacP atmP atm
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the pressure difference between poi
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Chapter 1 | 27Solution The reading
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Other Pressure Measurement DevicesA
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Chapter 1 | 31EXAMPLE 1-8Measuring
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Chapter 1 | 33Performing the integr
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Keep in mind that the solutions you
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Chapter 1 | 37which is an exact mat
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Chapter 1 | 39SUMMARYIn this chapte
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1-23C What is a steady-flow process
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60 NP atm = 95 kPam P = 4 kgChapter
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unknown density is poured into one
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1-96 The average temperature of the
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Chapter 1 | 491-112E Consider a U-t
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Chapter 2ENERGY, ENERGY TRANSFER, A
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Now if asked to name the energy tra
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Some Physical Insight to Internal E
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uranium-235 atom absorbs a neutron
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gz b E # mech m # e mech m # a P
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A process during which there is no
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Heat and work are directional quant
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Chapter 2 | 65Solution A well-insul
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EXAMPLE 2-7Power Transmission by th
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EXAMPLE 2-8Power Needs of a Car to
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erty is the total energy. Note that
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Chapter 2 | 73of a system during a
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E in E out ¢E systemChapter 2
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Chapter 2 | 777 cents per kWh, dete
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all resistance heaters is 100 perce
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the food to the energy consumed by
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converted entirely from one mechani
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Chapter 2 | 85Then the rate at whic
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usually grouped as hydrocarbons (HC
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Chapter 2 | 89a certain amount of a
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mechanical energy, and thus electri
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Chapter 2 | 93In solids, heat condu
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Chapter 2 | 95In general, both e an
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The energy flow rate associated wit
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2-23C What is the caloric theory? W
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this escalator. What would your ans
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espectively. If the pressure rise o
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700 W/m 2 and the surrounding air t
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The water flow rate through the pum
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2-141 The roof of an electrically h
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166 | ThermodynamicsThe movingbound
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168 | Thermodynamicscompression pro
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170 | ThermodynamicsEXAMPLE 4-3Isot
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172 | Thermodynamicsthe gas, and (c
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174 | ThermodynamicsGeneral Q - W =
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176 | ThermodynamicsUse actual data
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178 | ThermodynamicsVacuumP = 0W =
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180 | ThermodynamicsAIRm = 1 kg300
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182 | ThermodynamicsAIRT, Ku, kJ/kg
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184 | ThermodynamicsAIR at 300 Kc v
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186 | ThermodynamicsEXAMPLE 4-9Heat
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188 | ThermodynamicsP, kPa35023AIRF
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190 | ThermodynamicsFor solids, the
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⎫ ⎪⎬⎪⎭⎫⎪⎬⎪⎭192
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194 | ThermodynamicsA 300-Wrefriger
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196 | Thermodynamicsdays.) Although
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198 | ThermodynamicsTABLE 4-3The ra
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200 | ThermodynamicsSolution A pers
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202 | Thermodynamics4-7 A piston-cy
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204 | Thermodynamics4-30 A well-ins
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206 | Thermodynamics(Table A-2b), a
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208 | Thermodynamicsa rate of 100 b
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210 | Thermodynamicsof carbohydrate
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212 | ThermodynamicsQHePV n = const
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214 | Thermodynamicsthe entire air
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216 | Thermodynamics4-149 The speci
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218 | Thermodynamicsduring vacuum c
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220 | Thermodynamics2 kgH 216 kgO 2
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222 | Thermodynamicsm in = 50 kgWat
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224 | ThermodynamicsIt states that
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226 | Thermodynamicswhere A jet pD
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228 | ThermodynamicsThe fluid enter
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230 | ThermodynamicsFIGURE 5-17Many
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232 | ThermodynamicsCVW˙eW˙shFIGU
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234 | ThermodynamicsEXAMPLE 5-4Dece
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236 | ThermodynamicsDividing by the
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238 | ThermodynamicsAnalysis We tak
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240 | Thermodynamicsu 1 = 94.79 kJ/
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242 | Thermodynamics50°CFluid B70
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244 | ThermodynamicsR-134a. .Qw,in
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246 | ThermodynamicsSubstituting th
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248 | Thermodynamicsone of these wi
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250 | Thermodynamicssince the initi
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252 | ThermodynamicsThus,andv 2 0.
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254 | Thermodynamicsenergy per unit
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256 | Thermodynamicsunsteady-flow p
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258 | Thermodynamics5-15 Air enters
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260 | ThermodynamicsTurbines and Co
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262 | Thermodynamicsby the incoming
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264 | Thermodynamicsthe furnace. Ai
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266 | Thermodynamicsmass flow rate
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268 | Thermodynamicstank exists in
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270 | Thermodynamicsis allowed to e
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272 | Thermodynamicsfind the simple
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274 | Thermodynamicsenters the buil
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276 | Thermodynamicsopened, and air
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278 | Thermodynamics5-212 Refrigera
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280 | ThermodynamicsHOTCOFFEEHeatFI
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282 | ThermodynamicsWATERWorkFIGURE
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284 | ThermodynamicsorIt can also b
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286 | Thermodynamicsthe cycle, even
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288 | ThermodynamicsSurrounding med
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290 | ThermodynamicsFIGURE 6-23When
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292 | Thermodynamicsheat to the hou
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294 | ThermodynamicsSystem boundary
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296 | ThermodynamicsINTERACTIVETUTO
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298 | Thermodynamics20°CHeat5°C20
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300 | ThermodynamicsEnergysourceat
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302 | Thermodynamics1Irrev.HEHigh-t
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304 | Thermodynamicshave the same e
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306 | ThermodynamicsHigh-temperatur
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308 | ThermodynamicsQuantity versus
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310 | ThermodynamicsWarm environmen
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312 | ThermodynamicsTABLE 6-1Typica
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314 | ThermodynamicsCoolairWarmairR
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316 | Thermodynamicswhere W net,out
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318 | Thermodynamicsbetween the tem
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320 | Thermodynamics·120 kPax = 0.
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322 | ThermodynamicsIf the air surr
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324 | ThermodynamicsSpecial Topic:
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326 | Thermodynamics°F temperature
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328 | Thermodynamics$800 more to in
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330 | ThermodynamicsIf heat is supp
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332 | ThermodynamicsReversiblecycli
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334 | ThermodynamicsT∆S = S 2 - S
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336 | ThermodynamicsProcess 1-2(rev
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338 | ThermodynamicsSurroundings∆
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T340 | ThermodynamicsP 1 s 1 ≅ sT
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342 | ThermodynamicsEXAMPLE 7-4Entr
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344 | ThermodynamicsThe power outpu
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346 | ThermodynamicsTT HT L4A1 2W n
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348 | ThermodynamicsW shHOT BODY80
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350 | Thermodynamicsis highly irrev
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352 | ThermodynamicsEXAMPLE 7-7Effe
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354 | ThermodynamicsThen the power
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356 | ThermodynamicsandT 2 P 2s 2
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358 | ThermodynamicsIsentropic Proc
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360 | ThermodynamicsThe quantity T/
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362 | ThermodynamicsT, RT 2 = 780 R
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364 | ThermodynamicsIn gas power pl
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366 | ThermodynamicsP 1 , T 1TURBIN
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368 | ThermodynamicsPP 22Work saved
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370 | ThermodynamicsThe compressor
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372 | ThermodynamicsT,°CP 1 = 3 MP
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374 | ThermodynamicsEXAMPLE 7-15Eff
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376 | ThermodynamicsT, KP 1 = 200 k
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378 | ThermodynamicsEntropy Change
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380 | ThermodynamicsS inMassHeatSys
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382 | Thermodynamicsor, in the rate
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384 | ThermodynamicsT,°C4501Thrott
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386 | Thermodynamics(c) The entropy
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388 | ThermodynamicsSubstituting, t
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390 | Thermodynamicsat 100°C while
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392 | ThermodynamicsCompressor: 125
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394 | ThermodynamicsThen the mass f
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396 | ThermodynamicsW electricMotor
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398 | ThermodynamicsOutsideairWallA
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400 | Thermodynamicsambient in a li
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402 | ThermodynamicsPROBLEMS*Entrop
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404 | Thermodynamicsthis problem. L
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406 | Thermodynamics7-62C Starting
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408 | Thermodynamics7-91 Liquid wat
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410 | Thermodynamicstemperature of
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412 | Thermodynamics7-136E In a pro
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414 | Thermodynamicsfull load, and
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416 | Thermodynamics7-174 Consider
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418 | Thermodynamicsare 104°C and
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420 | Thermodynamicswater pipe heat
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422 | Thermodynamicsisentropic effi
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424 | ThermodynamicsAIR25°C101 kPa
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426 | Thermodynamicsm⋅⋅W max =
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428 | ThermodynamicsAtmosphericairP
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430 | ThermodynamicsIRON200°C27°C
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432 | Thermodynamicsof heat to the
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434 | ThermodynamicsFor a heat engi
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436 | Thermodynamicswhen the direct
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438 | ThermodynamicsEnergy:Exergy:e
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440 | ThermodynamicsThe properties
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442 | ThermodynamicsHeattransferEnt
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444 | ThermodynamicsThis equation c
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446 | ThermodynamicsOutersurroundin
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448 | ThermodynamicsBrick27°Cwall0
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450 | ThermodynamicsThat is, if the
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452 | Thermodynamics(b) The reversi
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454 | Thermodynamics(a) Noting that
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456 | ThermodynamicsThe useful work
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458 | ThermodynamicsWX workm ic iSu
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460 | Thermodynamicscold stream, pr
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462 | Thermodynamics(c) The second-
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464 | ThermodynamicsAssumptions 1 A
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466 | Thermodynamics“Now I’m in
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468 | ThermodynamicsI have only jus
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470 | ThermodynamicsExergytransferb
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472 | Thermodynamics8-21 How much o
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474 | Thermodynamicsactivated to st
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476 | Thermodynamics8-66E Refrigera
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478 | Thermodynamics8-87 Ambient ai
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480 | Thermodynamicsof the inner an
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482 | Thermodynamicssteam. Neglecti
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484 | Thermodynamics8-137 An adiaba
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Chapter 9GAS POWER CYCLESTwo import
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Chapter 9 | 489FIGURE 9-4An automot
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Isothermalcompressorq out43Isentrop
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oom temperature (25°C, or 77°F).
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Initially, both the intake and the
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and the specific heat ratio. This i
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Chapter 9 | 499P 3 v 3T 3 P 2v 2T 2
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We now define a new quantity, the c
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Chapter 9 | 503Process 2-3 is a con
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or any kind of porous plug with a h
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have long been of only theoretical
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wherer p P 0.72(9-18)P 1 0.6Chapte
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2. Increasing the efficiencies of t
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h C w s h 4a2s h 1(9-19)2a4sw a h
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q regen,act h 5 h 2 (9-21)Chapter
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Chapter 9 | 517Discussion Note that
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If the number of compression and ex
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tion on the thermal efficiency is a
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emaining part of the energy release
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Discussion For those who are wonder
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Chapter 9 | 527Fuel nozzles or spra
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Chapter 9 | 529EXAMPLE 9-10Second-L
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Chapter 9 | 531use per vehicle in t
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Chapter 9 | 533Park in the GarageTh
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Chapter 9 | 535acceleration. Using
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Chapter 9 | 537pistons, and prevent
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Chapter 9 | 539PROBLEMS*Actual and
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modeled as polytropic with a polytr
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9-84 A gas-turbine power plant oper
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9-111 Repeat Problem 9-110 using ar
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9-137 Repeat Problem 9-136 using co
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maximum? At what pressure ratio doe
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Chapter 10VAPOR AND COMBINED POWER
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This problem could be eliminated by
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or,wherew pump,in v 1P 2 P 1 2h 1
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558 | ThermodynamicsTIDEAL CYCLETIr
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560 | ThermodynamicsTurbine work ou
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562 | ThermodynamicsT21Criticalpoin
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564 | ThermodynamicsTherefore, the
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566 | ThermodynamicsTThe reheat cyc
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568 | ThermodynamicsandOpen Feedwat
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570 | Thermodynamicswherey m # 6>m
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572 | ThermodynamicsSome steam leav
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574 | ThermodynamicsDiscussion This
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576 | ThermodynamicsThus,andq in 1
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578 | ThermodynamicsTherefore, the
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580 | Thermodynamics3BoilerExpansio
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582 | Thermodynamicscycle and thus
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584 | Thermodynamicsin Fig. 10-24.
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586 | ThermodynamicsSteam cycle:(a)
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588 | ThermodynamicsT2 3BoilerMercu
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590 | ThermodynamicsPROBLEMS*Carnot
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592 | Thermodynamics410 kPa. Isobut
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594 | ThermodynamicsRegenerative Ra
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596 | Thermodynamics10-58 Reconside
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598 | ThermodynamicsCombined Gas-Va
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600 | Thermodynamics120 MW. Steam e
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602 | Thermodynamicsvaried from 0.5
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604 | Thermodynamicsan engineering
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708 | ThermodynamicsSUMMARYA mixtur
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710 | Thermodynamics13-21C How is t
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712 | ThermodynamicsThe mixture ent
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714 | Thermodynamics13-84 A rigid t
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Chapter 14GAS-VAPOR MIXTURES AND AI
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elow 50°C. Therefore, the enthalpy
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Chapter 14 | 721Analysis (a) The pa
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Chapter 14 | 723starts condensing.
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on this principle is called a sling
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Chapter 14 | 727EXAMPLE 14-4The Use
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the environment is close to 100 per
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Heating with HumidificationProblems
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The cooling process with dehumidify
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Chapter 14 | 735EXAMPLE 14-7Evapora
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Chapter 14 | 737Analysis We take th
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Chapter 14 | 739Properties The enth
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Chapter 14 | 741REFERENCES AND SUGG
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14-47 Reconsider Prob. 14-46. Deter
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equired results. Plot the required
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WARMWATER60 kg/s40°CAIRINLET1 atmT
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AIRCooling coilsCondensateFIGURE P1
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Chapter 15CHEMICAL REACTIONSIn the
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Chapter 15 | 753TABLE 15-1A compari
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not required.) However, notice that
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In actual combustion processes, it
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Chapter 15 | 759Assumptions 1 The f
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Chapter 15 | 761The combustion equa
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ing which chemical energy is releas
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C 8 H 18 a th 1O 2 3.76N 2 2 S 8C
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Q out a N r 1h° f h h°2 r1555
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Chapter 15 | 769The h - f ° of liq
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H prod H react (15-16)Chapter 15 |
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Chapter 15 | 773which is lower than
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If a gas mixture is at a relatively
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Chapter 15 | 777EXAMPLE 15-10Second
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Chapter 15 | 779(a) the heat transf
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Chapter 15 | 781cal reactions, the
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Chapter 15 | 783In the absence of a
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15-42 Determine the enthalpy of com
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Chapter 15 | 78715-65E A constant-v
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air used, and (c) the volume flow r
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where C is a constant whose value d
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Chapter 16CHEMICAL AND PHASE EQUILI
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The differential of the Gibbs funct
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where g - * (T) represents the Gibb
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Chapter 16 | 799Analysis This is a
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moles of the reactants and increase
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Chapter 16 | 803EXAMPLE 16-4Effect
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Chapter 16 | 805EXAMPLE 16-5Equilib
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calculating the h of a reaction fro
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What happens if g f g g ? Obviousl
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two sides of a water-air interface
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where is the solubility. Expressin
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Chapter 16 | 815EXAMPLE 16-11Compos
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Chapter 16 | 817PROBLEMS*K P and th
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Simultaneous Reactions16-38C What i
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16-83 A constant-volume tank contai
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Chapter 17COMPRESSIBLE FLOWFor the
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stagnation pressure, stagnation den
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Chapter 17 | 827Disregarding potent
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at constant velocity in still air m
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Chapter 17 | 831TABLE 17-1Variation
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increase as the flow area of the du
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The ratio of the stagnation to stat
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Now we begin to reduce the back pre
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Another parameter sometimes used in
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Chapter 17 | 841Solution Nitrogen g
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Chapter 17 | 843P 0V i ≅ 0ThroatP
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Chapter 17 | 845(b) Since the flow
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The conservation of energy principl
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Chapter 17 | 849FIGURE 17-33Schlier
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Chapter 17 | 851The fluid propertie
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1 V 1,n A r 2 V 2,n A S r 1 V 1,n
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u, degrees504030201010 5Ma → 1 32
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where we must be careful to measure
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Chapter 17 | 859Analysis Because of
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1 V 1 r 2 V 2 (17-50)Chapter 17 |
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except for the narrow Mach number r
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Chapter 17 | 865Therefore, sonic co
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Also,P 0 P 0 P P* a 1 k 1 k>1k12M
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Chapter 17 | 869The maximum value o
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Analysis We denote the entrance, th
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Nozzles whose flow area decreases i
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17-24E Steam flows through a device
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17-77C Are the isentropic relations
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17-115E Steam enters a converging n
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17-154 Air is flowing in a wind tun