Apostila aeronautica tecologista jr mecanica termo e trans cal

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r= ⌘Otto = 1

Wliq =1 QH

QL QH

QH = mar .cV (T3

T2 )

QL = mar .cV (T4

T1 )

⌘Otto =

⌘Otto = 1

mar .cV (T4 mar .cV (T3

⌘Otto = 1

k=

T1 T1T4 1 T2 T2T3 1

cp cv

T1 ) T2 )

V4 V1 = V2 V3 1

( VV12 )k 1

=1

1 (r)k

1


⌘Brayton = 1

⌘Brayton =

Wliq QH QL = =1 QH QH

QL QH

L

QL =

H(4!1) = mar .cp (T4

T1 )

H(2!3) = mar .cp (T3

T2 )

H

QH =

T1 T2


Q=

H+

0 = (3160000 Q=

H+

Ec +

Ep + W

0 = 2((3160000

Ec +

Ep + W

102 2675000) + +W 2 2675000) +

102 )+W 2

W = 970,1

H

L


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