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RADIATION AND COMBUSTION PHENOMENA

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Presentation on theme: "RADIATION AND COMBUSTION PHENOMENA"— Presentation transcript:

1 RADIATION AND COMBUSTION PHENOMENA
PROF. SEUNG WOOK BAEK DEPARTMENT OF AEROSPACE ENGINEERING, KAIST, IN KOREA ROOM: Building N7-2 #3304 TELEPHONE : 3714 Cellphone : 010 – TA : Jonghan Won ROOM: Building N7-2 # 3315 TELEPHONE : 3754 Cellphone :

2 RADIATIVE HEAT TRANSFER
GAS RADIATION EXAMPLE STEADY 1D CONDUCTION+RADIATION GENERAL PRINCIPLE PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

3 RADIATIVE HEAT TRANSFER
GAS RADIATION FROM ④ CONSTITUTION GOVERNING EQUATION FOR R = Const , k = Const , TOTAL ENERGY , RADIATION PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

4 RADIATIVE HEAT TRANSFER
GAS RADIATION INTRODUCE OPERATE TOTAL ENERGY WITH IN TERMS OF PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

5 RADIATIVE HEAT TRANSFER
GAS RADIATION LINEARIZE WHERE THEN PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

6 RADIATIVE HEAT TRANSFER
GAS RADIATION GENERAL SOLUTION NEED BOUNDARIES PROBLEMS OBTAIN LIMITS OF ⑤ FOR AND (THIN AND THICK GAS) OBTAIN LIMITS OF ⑥ FOR AND (COLD AND HOT GAS) PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

7 RADIATIVE HEAT TRANSFER
GAS RADIATION BOUNDARY EFFECTS APPROXIMATE AND ON THE BASIS OF HEMISPHERICAL ISOTROPY PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

8 RADIATIVE HEAT TRANSFER
GAS RADIATION PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

9 RADIATIVE HEAT TRANSFER
GAS RADIATION WITH HEMISPHERICAL ISOTROPY NOW PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

10 RADIATIVE HEAT TRANSFER
GAS RADIATION IN TERMS OF J, THE RADIATIVE ENERGY BALANCE BECOMES RECALL FOR THIN GAS BETWEEN TWO PARALLEL PLATES PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

11 RADIATIVE HEAT TRANSFER
GAS RADIATION SOLVE FOR AND THEN PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

12 RADIATIVE HEAT TRANSFER
GAS RADIATION REARRANGE IN TERMS OF OR PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

13 RADIATIVE HEAT TRANSFER
GAS RADIATION OR OR CONSTITUTION OF THIN GAS BETWEEN TWO PARALLEL PLATES WHERE PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

14 RADIATIVE HEAT TRANSFER
GAS RADIATION LINEARIZED THIN GAS FOR PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

15 RADIATIVE HEAT TRANSFER
GAS RADIATION EXAMPLE LINEARIZED THIN GAS BETWEEN TWO PARALLEL PLATES INTRODUCE PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

16 RADIATIVE HEAT TRANSFER
GAS RADIATION SOLUTION BC’S THEN PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

17 RADIATIVE HEAT TRANSFER
GAS RADIATION WHICH MAY BE REARRANGED AS PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

18 RADIATIVE HEAT TRANSFER
GAS RADIATION EXAMPLE RADIATION AFFECTED AERODYNAMIC HEATING CONSTITUTION PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

19 RADIATIVE HEAT TRANSFER
GAS RADIATION GOVERNING EQUATION ; FOR THIN GAS WHERE PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

20 RADIATIVE HEAT TRANSFER
GAS RADIATION WHERE THEN GOVERNING EQUATION PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

21 RADIATIVE HEAT TRANSFER
GAS RADIATION LINEARIZED REARRANGE IN TERMS OF PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

22 RADIATIVE HEAT TRANSFER
GAS RADIATION LET THEN PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

23 RADIATIVE HEAT TRANSFER
GAS RADIATION INSULATED WALL PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

24 RADIATIVE HEAT TRANSFER
GAS RADIATION NOTE LINEARIZE PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

25 RADIATIVE HEAT TRANSFER
GAS RADIATION INTRODUCE AND EVALUATE INSERT INTO BC LET (ADIABATIC WALL TEMPERATURE) PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

26 RADIATIVE HEAT TRANSFER
GAS RADIATION RECALL , BECAUSE IT INCLUDES THEN PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

27 RADIATIVE HEAT TRANSFER
GAS RADIATION REARRANGE SOLVE FOR PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER

28 RADIATIVE HEAT TRANSFER
GAS RADIATION AS RECALLING OR WHICH IS IDENTICAL TO THE RESULT OBTAINED BEFORE (File #4, slide 15) PROPULSION AND COMBUSTION LABORATORY RADIATIVE HEAT TRANSFER


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