3532IES-7. ANS. (C) IES-8. ANS. (C) IES-9. ANS. (C) IES-10. ANS....

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2

IES-7. Ans. (c)

IES-8. Ans. (c)

IES-9. Ans. (c)

IES-10. Ans. (a)

IES-11. Ans. (d)

IES-12. Ans. (d)

IES-13. Ans. (b)

σ

π

2

4

2

4

E

r T

=

=

=

×

=

4

1

4000

4

E

AT

IES-14. Ans. (c)

A

A

A

;

1

(

)

π

4

4

2000

×

B

B B

IES-15. Ans. (a)

4

4

E

T

300

1

εσ

4

1

1

=

=

=

=

Emissive power ( )

IES-16. Ans. (d)

E

T or

900

81

2

2

IES-17. Ans. (d) Irradiation on a small test surface placed inside a hollow black spherical

chamber = σT

4

= 5.67 × 10

-8

× 600

4

= 7348 W/m

2

IES-18. Ans. (a) Rate of emission of radiative flux

=

σ

T

4

3

8

4

or

7.35 10

×

=

5.67 10

×

×

T

or

T

=

600 K

IES-19. Ans. (c)

IES-20. Ans. (b)

Heat transfer through solid

Fourier’s law of heat

conduction

Heat transfer from hot surface to

surrounding fluid

Newton’s law of cooling

Heat transfer in boiling liquid

Convection heat transfer

Heat transfer from one body to

Radiation heat

Page 91 of 97

another transfer separated in

space

IES-21. Ans. (a)

IES-22. Ans. (b)

IES-23. Ans. (b)

IES-24. Ans. (d) Total emissive power is defined as the total amount of radiation emitted

by a body per unit time

. .

0 3 150 (12 3) 300 (25 12) 0[ ]

i e

E

=

E d

λ

λ λ

= × +

×

+

×

+

α

=

× +

×

=

+

=

150 9 300 13 1350 3900 5250 W/m

IES-25. Ans. (c)

IES-26. Ans. (c)

IES-27. Ans. (b) As per Wien's law,

λ

1 1

T

=

λ

2 2

T or

5800 0.5

×

=

λ

2

×

573

IES-28. Ans. (c)

IES-29. Ans. (c) We know that, I =

E

IES-30. Ans. (c)

IES-31. Ans. (c) All the emission from one plate will cross another plate. So Shape Factor

in one.

IES-32. Ans. (b) A

1

F

1 – 2

= A

2

F

2 – 1

or

F

2 – 1

=

1

1 2

A

.

A

F

=

6

0.1

4

×

= 0.15

IES-33. Ans. (c)

2 1

2 2

2 2

2 1