Q2.The numerical solution of the Falknar-Scan Equation f' 0.0 0.0000000 0.000000 f" 0.363600 f + ff +B[1- (f )’]= 0 0.2 0.0093914 0.093905 0.4 0.0375492 0.187605 0.6 0.0843856 0.280575 0.355306 about a plate with pressure gradient are given in Table. Free stream velocitv of air is 10 m/s. 0.327254 0.301734 0.291190 0.8 0.1496745 0.371963 1.0 0.2329900 0.460632 0.284379 0.270565 1.2 0.3336572 0.545246 Calculate: 1.4 0.4507234 0.624386 0.269692 1.6 0.5829560 0.696699 0.252487 1.8 0.7288718 0.761057 a) Boundary laver thickness, O(x), dispalecement thickness &*(x) and the local friction coefficient. C:(x). b) Drag force acting on the plate with 80 in length and 40 cm in width 0.240445 2.0 0.8867962 0.766694 0.225669 2.2 1.0549463 0.793303 2.4 1.2315267 0.811065 0.210580 0.167561 2.6 1.4148231 0.830601 0.128613 Note: The density and viscosity, of air is 1.12 kg/m³ and 1.56x10-5 m?/s respectively. f' =u/U 2.8 1.6032823 0.852875 3.0 1.7955666 0.879054 0.095114 0.067711 0.0463 70 3.2 1.9905 796 0.890365 3.4 2.1874658 0.907970 3.6 2.3855888 0.922888 3.8 2.5844972 0.965944 4.0 2.7838848 0.98770 4.2 2.9835535 0.998818 4.4 3.183380 S 0,999396 0.030535 0.019329 0.011759 0.006874 0.003861 0.002084 5.0 3.7832324 0.999936 0.000258
Q2.The numerical solution of the Falknar-Scan Equation f' 0.0 0.0000000 0.000000 f" 0.363600 f + ff +B[1- (f )’]= 0 0.2 0.0093914 0.093905 0.4 0.0375492 0.187605 0.6 0.0843856 0.280575 0.355306 about a plate with pressure gradient are given in Table. Free stream velocitv of air is 10 m/s. 0.327254 0.301734 0.291190 0.8 0.1496745 0.371963 1.0 0.2329900 0.460632 0.284379 0.270565 1.2 0.3336572 0.545246 Calculate: 1.4 0.4507234 0.624386 0.269692 1.6 0.5829560 0.696699 0.252487 1.8 0.7288718 0.761057 a) Boundary laver thickness, O(x), dispalecement thickness &*(x) and the local friction coefficient. C:(x). b) Drag force acting on the plate with 80 in length and 40 cm in width 0.240445 2.0 0.8867962 0.766694 0.225669 2.2 1.0549463 0.793303 2.4 1.2315267 0.811065 0.210580 0.167561 2.6 1.4148231 0.830601 0.128613 Note: The density and viscosity, of air is 1.12 kg/m³ and 1.56x10-5 m?/s respectively. f' =u/U 2.8 1.6032823 0.852875 3.0 1.7955666 0.879054 0.095114 0.067711 0.0463 70 3.2 1.9905 796 0.890365 3.4 2.1874658 0.907970 3.6 2.3855888 0.922888 3.8 2.5844972 0.965944 4.0 2.7838848 0.98770 4.2 2.9835535 0.998818 4.4 3.183380 S 0,999396 0.030535 0.019329 0.011759 0.006874 0.003861 0.002084 5.0 3.7832324 0.999936 0.000258
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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![Q2.The numerical solution of the Falknar-Scan Equation
f'
0.0 0.0000000 0.000000
f"
0.363600
f + ff + B[1- (f )’]= 0
0.2 0.0093914 0.093905
0.4 0.0375492 0.187605
0.6 0.0843856 0.280575
0.355306
0.327254
0.301734
0.291190
about a plate with pressure gradient are given in Table.
Eree stream velocity of air is. 10 m/s.
0.8 0.1496745 0.371963
1.0 0.2329900 0.460632
1.2 0.3336572 0.545246
0.284379
0.270565
Calculate:
1.4 0.4507234 0.624386
0.269692
1.6 0.5829560 0.696699
1.8 0.7288718 0.761057
2.0 0.8867962 0.766694
0.252487
0.240445
a) Boundary laver thickness, 8(x), dispalecement thickness &*(x) and the
0.225669
local friction coefficient. C (x).
b) Drag force acting on the plate with 80 in length and 40 cm in width
2.2 1.0549463 0.793303
2.4 1.2315267 0.811065
0.210580
0.167561
2.6 1.4148231 0.830601
0.128613
Note: The density and viscosity of air is 1.12 kg/m and 1.56x10-s m²/s
respectively. f' =u/U
2.8 1.6032823 0.852875
3.0 1.7955666 0.879054
0.095114
0.067711
0.046370
3.2 1.9905796 0.890365
3.4 2.1874658 0.907970
3.6 2.3855888 0.922888
0.030535
0.019329
0.011759
3.8 2.5844972 0.965944
4.0 2.7838848 0.98770
4.2 2.9835535 0.998818
4.4 3.183380S ,999396
5.0 3.7832324 0.999936
0.006874
0.003861
0.002084
0.000258](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2Fb628b176-4f73-4356-aac5-d447d39ac4aa%2Fb56a0604-617c-4848-9116-7ca4ee61ee6c%2F762bt5n_processed.png&w=3840&q=75)
Transcribed Image Text:Q2.The numerical solution of the Falknar-Scan Equation
f'
0.0 0.0000000 0.000000
f"
0.363600
f + ff + B[1- (f )’]= 0
0.2 0.0093914 0.093905
0.4 0.0375492 0.187605
0.6 0.0843856 0.280575
0.355306
0.327254
0.301734
0.291190
about a plate with pressure gradient are given in Table.
Eree stream velocity of air is. 10 m/s.
0.8 0.1496745 0.371963
1.0 0.2329900 0.460632
1.2 0.3336572 0.545246
0.284379
0.270565
Calculate:
1.4 0.4507234 0.624386
0.269692
1.6 0.5829560 0.696699
1.8 0.7288718 0.761057
2.0 0.8867962 0.766694
0.252487
0.240445
a) Boundary laver thickness, 8(x), dispalecement thickness &*(x) and the
0.225669
local friction coefficient. C (x).
b) Drag force acting on the plate with 80 in length and 40 cm in width
2.2 1.0549463 0.793303
2.4 1.2315267 0.811065
0.210580
0.167561
2.6 1.4148231 0.830601
0.128613
Note: The density and viscosity of air is 1.12 kg/m and 1.56x10-s m²/s
respectively. f' =u/U
2.8 1.6032823 0.852875
3.0 1.7955666 0.879054
0.095114
0.067711
0.046370
3.2 1.9905796 0.890365
3.4 2.1874658 0.907970
3.6 2.3855888 0.922888
0.030535
0.019329
0.011759
3.8 2.5844972 0.965944
4.0 2.7838848 0.98770
4.2 2.9835535 0.998818
4.4 3.183380S ,999396
5.0 3.7832324 0.999936
0.006874
0.003861
0.002084
0.000258
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