Air at 1 MPa and 600 °C enters the convergent Lule shown in Figure 2 at a speed of 150 m/s.Mass flow in this Lule with a throat area of 50 cm? (a) for 0.7 MPa, (b) find 0.4 MPa for counter pressure values. Cp= 1.005 kJ / kg.K and K=1.4 is. AIR P 1 MPa P convergent nozzle T; = 600°C V; = 150 m/s A, = 50 cm2
Air at 1 MPa and 600 °C enters the convergent Lule shown in Figure 2 at a speed of 150 m/s.Mass flow in this Lule with a throat area of 50 cm? (a) for 0.7 MPa, (b) find 0.4 MPa for counter pressure values. Cp= 1.005 kJ / kg.K and K=1.4 is. AIR P 1 MPa P convergent nozzle T; = 600°C V; = 150 m/s A, = 50 cm2
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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Transcribed Image Text:Air at 1 MPa and 600 °C enters the convergent Lule shown in Figure 2 at a speed of 150 m/s.Mass
flow in this Lule with a throat area of 50 cm?
(a) for 0.7 MPa,
(b) find 0.4 MPa for counter pressure values.
Cp= 1.005 kJ / kg.K and K=1.4 is.
AIR
P
1 MPa
P
convergent
nozzle
T; = 600°C
V; = 150 m/s
A, = 50 cm2

Transcribed Image Text:TABLO 12-2
Bazı ideal gazların izentropik akışında kritik basınç, kritik sıcaklık ve kritik yoğunluk oranları.
Sıcak yanma
Tek atomlu
Kızgın buhar,
k = 1.3
ürünleri,
Hava,
k = 1.33
k = 1.4
gazlar,
k = 1.667
0.5457
0.5404
0.5283
0.4871
0.8696
0.8584
0.8333
0.7499
To
0.6276
0.6295
0.6340
0.6495
Po
TABLE A-13
k- 1.4 değerine sahip ideal gaz için bir-boyutlu izentropik
sıkıştırılabilir akış fonksiyonları
Ma
AlA*
PIP.
Ma*
plpo
TITO
1.0000
1.0000
1.0000
0.1094
0.2182
0.9950
0.9980
0.9921
0.9823
0.1
5.8218
0.9930
0.2
2.9635
2.0351
0.9725
0.9803
0.3
0.3257
0.9395
0.9564
0.9690
0.9524
0.9328
0.9107
0.8865
0.4313
0.5345
0.4
1.5901
0.8956
0.9243
1.3398
1.1882
1.0944
0.5
0.8430
0.8852
0.7840
0.7209
0.6560
0.6
0.6348
0.8405
0.7
0.7318
0.7916
0.7400
0.8
0.8251
1.0382
0.9
0.9146
1.0089
0.5913
0.6870
0.8606
1.0000
1.1583
1.0
1.0000
0.5283
0.6339
0.8333
1.0304
1.2
1.4
0.4124
0.5311
0.7764
1.2999
1.4254
1.1149
0.3142
0.4374
0.7184
1.6
1.2502
0.2353
0.3557
0.6614
1.4390
1.6875
0.1740
0.1278
1.5360
0.6068
0.5556
0.5081
0.4647
1.8
0.2868
0.2300
0.1841
0.1472
2.0
2.2
1.6330
1.7179
2.0050
0.0935
2.4
1.7922
2.4031
0.0684
2.8960
3.5001
4.2346
2.6
1.8571
0.0501
0.1179
0.4252
0.3894
0.3571
2.8
1.9140
0.0368
0.0946
3.0
5.0
0.0272
0.0019
0.0760
1.9640
2.2361
25.000
0.0113
0.1667
2.2495
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