Page 22 - Numerical Analysis and Modelling in Geomechanics
P. 22

SURFACE DISPLACEMENTS OF AN AIRFIELD RUNWAY 3

































            Figure 1.1 Half section of camouflet showing the void and the eight zones.

            the  effect  of  the  depth  of  detonation  on  runway  deflection  when  a  downward
            vertical uniformly distributed load is applied to the runway surface.


                                 Camouflet characteristics
            The  characteristics  of  explosively  formed  craters  can  be  linked  directly  to
            dimensional analysis, statistical reasoning and scaling laws [9, 10, 15–22]. The
            most common relationship being “Hopkinson’s law”, which says that any scaled
            linear  dimension  L  (m)  of  the  crater  may  be  related  to  L/W 0.33  where  W  (kg),
            represents the mass of the equivalent yield of TNT of the explosive charge [18, 23].
            The factors determining the size and the shape of the crater are the mass of the
            explosive,  the  position  λ c  of  the  point  of  detonation  and  the  medium  within
            which the detonation takes place [16, 17]. The value of λ  (m) is obtained from
                                                           c
            the location of the point of detonation (m), which is negative below the runway
            surface, divided by W 0.33 . If the detonation occurs below the air-ground interface
            (λ <0), then the resulting crater is a camouflet if λ =−1.388. The way in which
                                                     c
             c
            the subgrade reacts to the detonation depends upon the medium within which the
            detonation  takes  place.  If  the  medium  is  rock  the  detonation  forms  a  void  and
            pushes  up  a  cylindrically  shaped  column  of  broken  rock  which  later  collapses
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