THERMODYNAMICSUPVOTE WILL BE GIVEN. PLEASE WRITE THE COMPLETE SOLUTIONS. NO LONG EXPLANATION NEEDED. BOX THE FINAL ANSWER AND USE 3 DECIMAL PLACES. DRAW PV-TS Diagrams.A scuba tank contains 1.5 kg of air. The air in the tank is initially at 15°C. The tank is left near an engine exhaust line, and the tank's pressure doubles. Determine (a) the final temperature; (b) the change in internal energy; (c) the heat added. (d) ΔS. please see the image attached for the constants GasAcetyleneAirAmmoniaArgonn-ButaneCarbon DioxideCarbon MonoxideChlorineEthaneEthyleneHeliumHydrochloric AcidHydrogenHydrogen SulphideMethaneMethyl ChlorideNatural GasNeonNitric OxideNitrogenNitrous OxideOxygenC₂H₂Nh,ArC₂H₁₂CO₂соCLCH₂C.HHeHCIH₂H.SCH,CH₂CINeNON₂N.O0₂Formula26291739.958.1442870.93028436.5234.11650.519.520.1830284432MW1.09251.20450.71791.6612.48971.84171.16482.99441.2635Density(kg/m3)1.17440.16631.52730.08371.43340.66732.150.80340.841.29411.16481.84291.331R(Gas constant)kJ/(kg.k)0,320.2870 490.2060.1430.1890.2970.1170.2770.2962 0780.2284.1260.2430.5190.1650.4260.2770.2970.1890.261.4651.0092.190.5191.6540.8581.0170.4811.6161.6755.2340.8CpkJ/(kg.K)14.3191.0172.4831.0052.3450.9671.0340.9250.909CvkJ/(kg.K)1.1270.7211.6590.3111.490.660.7260.3621.3251.3733.1530.56710.1550.7821.8610.8381.8460.6910.7330.7060.6491.31.41.321.671.111.31.41.331.221.221.661.411.411.31.321.21.271.41.411.311.4Cp/CV y

Answered: Image /qna-images/answer/1cccb958-9b48-4222-b52f-c34bd36c5ddb.jpg

Answered: DRAW PV-TS Diagrams. A scuba tank…

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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THERMODYNAMICS

UPVOTE WILL BE GIVEN. PLEASE WRITE THE COMPLETE SOLUTIONS. NO LONG EXPLANATION NEEDED. BOX THE FINAL ANSWER AND USE 3 DECIMAL PLACES. DRAW PV-TS Diagrams.

A scuba tank contains 1.5 kg of air. The air in the tank is initially at 15°C. The tank is left near an engine exhaust line, and the tank's pressure doubles. Determine (a) the final temperature; (b) the change in internal energy; (c) the heat added. (d) ΔS.

please see the image attached for the constants

Gas
Acetylene
Air
Ammonia
Argon
n-Butane
Carbon Dioxide
Carbon Monoxide
Chlorine
Ethane
Ethylene
Helium
Hydrochloric Acid
Hydrogen
Hydrogen Sulphide
Methane
Methyl Chloride
Natural Gas
Neon
Nitric Oxide
Nitrogen
Nitrous Oxide
Oxygen
C₂H₂
Nh,
Ar
C₂H₁₂
CO₂
со
CL
CH₂
C.H
He
HCI
H₂
H.S
CH,
CH₂CI
Ne
NO
N₂
N.O
0₂
Formula
26
29
17
39.9
58.1
44
28
70.9
30
28
4
36.5
2
34.1
16
50.5
19.5
20.18
30
28
44
32
MW
1.0925
1.2045
0.7179
1.661
2.4897
1.8417
1.1648
2.9944
1.2635
Density
(kg/m3)
1.1744
0.1663
1.5273
0.0837
1.4334
0.6673
2.15
0.8034
0.84
1.2941
1.1648
1.8429
1.331
R
(Gas constant)
kJ/(kg.k)
0,32
0.287
0 49
0.206
0.143
0.189
0.297
0.117
0.277
0.296
2 078
0.228
4.126
0.243
0.519
0.165
0.426
0.277
0.297
0.189
0.26
1.465
1.009
2.19
0.519
1.654
0.858
1.017
0.481
1.616
1.675
5.234
0.8
Cp
kJ/(kg.K)
14.319
1.017
2.483
1.005
2.345
0.967
1.034
0.925
0.909
Cv
kJ/(kg.K)
1.127
0.721
1.659
0.311
1.49
0.66
0.726
0.362
1.325
1.373
3.153
0.567
10.155
0.782
1.861
0.838
1.846
0.691
0.733
0.706
0.649
1.3
1.4
1.32
1.67
1.11
1.3
1.4
1.33
1.22
1.22
1.66
1.41
1.41
1.3
1.32
1.2
1.27
1.4
1.41
1.31
1.4
Cp/CV y

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