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394


            References
            Moshaiov A.  and Latorre R.(1985) Temperature Distribution During Plate Bending by Torch Flame
            Heating, Journal of Ship Research 29: 1, pp. 1-1 1.
            Tsuji I.  and Okumura Y.(1977) A Study on Line Heating Process for Plate Bending of Ship Steels,
            Trans. The WestJapan SOC. Naval Architects 76, pp.149-160 (in  Japanese).
            Terasaki T.,  Kitamura N. and Nakai M.(1999)  Predictive muation for Thermal Cycle Generated by
            Line Heating Method, Trans. The WestJapan SOC. Naval Architects 99, pp.321-329 (in  Japanese).
            Beck J.V., Blackwell B. and St. Clair Jr., C. R.(1985) Inverse Heat Conduction, A Weley-Interscience
            Publication.

                           TABLE 1
             FLUX AND PRESSURE OF CHEMICAL SPECIES USED
                     IN THE L.I.F. EXPERIMENT                     (a) Z=12mm
                           flux (m’/sec)   pressure (ma)
                 NO         2.50~10~      98.07
                 02         2.83~10’      245.17
                 CIC        2.67~10’      196.13
                                                                  (b) Z4Omm


                                                      .I.     ..  ,   ~  . .   .  ..  . .  ..  ..  .  .
                                                                   (c) Z=28mm
                                       Corrrdnn Bma   Figure 3: Averaged temperature distributions of
              ICCD cmw 1
                                                                 gas flame





            I



                     Figure 1 : Optical system

                                                        :,I

                e  -   rn  .~  ,.   I/ .  .r  .   ,*     4W     50          50     0
              u    I      .L   ~            ,e
                           (a) t=2sec                   Distance from the stagnation point [mm]
                                                   Figure 4: Measured gas temperature distribution
                           \I
                                                   on  the  plane  1.5m upward  from  the  plate
                                                   surface for the case where Z=12m
                                            .*.
              -  =  =  *  1  0  1  1  *   .  1  *  *  *  ,  o  .  *  m  m  m  -  z
                           (b) t44sec                            TABLE 2
            Figure  2: Measured temperature distribution of   FLUX AM) PRESSURE OF CHEMICAL SPECIES USED
            gas flame in a transient state for the case where   IN THE SPOT HEATING EXPERIMENT
            z=20mm.
                                                                  flux (m’/sec)   pressure (KPa)
                                                        02           0.0        6.92~ IOs
                                                       CzHz        4.62~10’     5.76~10~
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