Formula MECH390

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  • 8/13/2019 Formula MECH390

    1/2

    Mech 390 Formula Sheet

    total energy, mass:

    V

    potkin dVgzuEEUE2

    2

    1V ,

    V

    dVm

    Closed systems:

    1stlaw, general form: WQdt

    dE , 121212 WQEE , WQdE

    reversible proc.:dt

    dVpQ

    dt

    dU ,

    2

    1

    1212 pdVQUU

    specific work / heat in rev. proc.: 2

    1

    1212 pdv

    m

    Ww , 1212

    2

    1

    1212 wuuTds

    m

    Qq

    2ndlaw 0 genk k

    k ST

    Q

    dt

    dS

    012 genk k

    k ST

    QSS

    Open systems:

    mass balance: out ein i mmdtdm

    mass flow: Am V

    1stlaw, general form: WQgzhmgzhmdt

    dE

    in

    iiii

    out

    eeee

    22

    2

    1

    2

    1VV , h=u+pv

    specific work / heat in rev. proc.: 2

    1

    1212 vdp

    m

    Ww

    2

    1

    1212 Tds

    m

    Qq

    2ndlaw: 0 genk k

    k

    in

    ii

    out

    ee ST

    Qsmsm

    dt

    dS

    Gibbs equation: pdvduTds , vdpdhTds

    Liquid-vapor two phase systems (saturated states):

    quality

    fg

    f

    fg

    f

    fg

    f

    fg

    f

    s

    ss

    u

    uu

    vv

    vv

    h

    hhx

    properties fgf xhhh , gf xvvxv 1 , fgf xuuu , fgf xsss

    Compressed liquid properties (approx.):

    spec. volume TvpTv f,

    spec. int. energy 00, uTTcTupTu f

    specific enthalpy TppTvThpTh satff ,

    entropy TspTs f,

    Incompressible liquids/solids (const. specific heat):

    thermal equation of state: .constv

    caloric eq. of state: 00 uTTcu 000 hppvTTch

    entropy:0

    0

    ln sT

    Tcs

  • 8/13/2019 Formula MECH390

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    Ideal gases:

    thermal equation of state: RTpv mRTpV RTp

    gas constant, spec. heats:M

    RR ,

    Kkmol

    kJ314.8R , Rcc vp ,

    v

    p

    c

    ck

    caloric equation of state: 00

    '' udTTcTuT

    T v 0

    0

    '' hdTTcThT

    T p

    for const. specific heats: 00

    uTTcuv

    00

    hTTchp

    entropy 1

    21

    0

    2

    0

    1122 ln,,p

    pRTsTspTspTs

    for const. specific heats: 1

    2

    1

    21122 lnln,,

    p

    pR

    T

    TcpTspTs p

    , 1

    2

    1

    21122 lnln,,

    v

    vR

    T

    TcvTsvTs v

    isentropic processes:

    1

    2

    1

    0

    2

    0

    1

    2

    exp

    exp

    Tp

    Tp

    RTs

    RTs

    p

    p

    r

    r , 1

    2

    1

    2

    Tv

    Tv

    v

    v

    r

    r

    for const. specific heats: .constpvk , .1 constTv k , .1

    constTp kk

    Carnot engines: heat engineH

    LCth

    T

    T1, , refrigerator

    1

    1,

    L

    HCR

    T

    TCOP , heat pump

    H

    LCHP

    T

    TCOP

    1

    1,

    Isentropic efficiency: compressorC

    revC

    Cw

    w, , turbine

    revT

    TT

    w

    w

    ,

    , nozzle2

    2

    rev

    NV

    V

    Speed of sound:s

    pa

    |

    in ideal gas: kRTa Mach number:

    a

    vM

    Mixtures of ideal gases:

    mole fraction:p

    p

    n

    nX mass fraction:

    M

    MX

    m

    mc

    molar/mass based properties, e.g. enthalpy: X hch Psychrometrics:

    humidity ratio:v

    v

    a

    v

    pp

    p

    m

    m

    622.0 relative humidity:

    Tpp

    sat

    v

    enthalpy, volume per unit mass of dry air: va hhh 1 p

    TR

    M

    Mv a

    v

    a

    11

    Combustion:

    1stlaw for open systems: WQhhNhhNnin

    RfR

    outPfPFuel

    00

    (steady state) where RR pThpThh ,,