with reference to fig1 and 2 of the drawings , in one of its simplest forms , the invention comprises an ordered array of materials comprising a first layer 2 of stainless steel material , which is positioned on an upper surface of a core layer 4 of aluminum material which , in turn , is positioned on an upper surface of a second layer 6 of stainless steel material . the layers 2 , 4 , and 6 are preferably pre - cut , round shaped flat discs of a diameter suitable for making a bonded composite blank of near net - shape for subsequent forming into a fry pan , fig7 . a perforated template 10 , as shown also in fig3 and 4 , is positioned on top of the first stainless steel layer 2 in the ordered stacked array of materials shown in fig1 and 2 . the perforated template 10 contains a plurality of spaced - apart throughholes 14 interspaced between closed flat portions 16 in the central area of the template 10 . the outer border area of the template 10 has no perforations . in a presently preferred embodiment , approximately 50 % of the surface area of the perforated template 10 contains open through holes 14 . this ratio of open through holes 14 to closed portions 16 , by surface area , may vary between about 25 - 75 % in the central area of the template 10 . presently , about a 50 % hole ratio appears to be very acceptable . the holes can be round or may be other shapes , such as , for example , rectangles , squares , hexagons and the like . in one present embodiment , shown in the drawings , the round hole diameter of each through hole 14 in the perforated template 10 is 0 . 287 inch in diameter and the spacing between holes is 0 . 375 inch from each hole center . the perforations 14 in the central portion are intended to form the bubbles 20 along the cooking surface of the cookware while the outer border ( without perforations ) is intended to form the area of the smooth sidewall of the cookware . fig2 schematically ( not to scale ) demonstrates the solid state bonding operation of the ordered array of one presently preferred embodiment which bonds the first stainless steel layer 2 to the core layer 4 of aluminum and the second , lower layer 6 of stainless steel . an axially applied force is imposed upon the stacked array , including the perforated template 10 , by way of an upper platen 12 or 12 ′ and a lower platen 8 under a pressure of between about 15 , 000 - 35 , 000 psi , wherein the axial force is applied in a normal 90 ° direction to the plane of the stacked array 10 , 2 , 4 , 6 . during the application of the pressure which ideally is around 20 , 000 psi , a heat is also applied between about 800 - 900 ° f . or , more broadly , 750 ° - 950 ° f ., for a period of time sufficient to achieve bonding between the stainless steel layer 2 , aluminum layer 4 , and stainless steel layer 6 . during the application of the temperature and pressure , the aluminum layer 4 thermally expands , forcing the first stainless steel layer 2 to expand into the through holes 14 of the perforated template 10 to form a plurality of dimples or bubbles 20 in the first stainless steel layer 2 . the template 10 is also formed preferably of stainless steel , which will not form a bond with the first stainless steel layer 2 during the application of pressure and temperature . thus , upon completion of the pressure and temperature bonding operation , when the force is removed , as shown in fig2 , the template 10 will not bond to the first layer of stainless steel 2 and can be reused in subsequent bonding operations . fig5 shows the flat blank after the bonding operation with the perforated template 10 removed from the bonded blank comprising the first stainless steel layer 2 bonded to the aluminum core layer 4 and the lower , second stainless steel layer 6 bonded to the core layer 4 . the raised dimples or bubbles 20 are shown on the thrilled blank 30 shown in fig2 and in fig5 . the round three - layer composite bonded blank 30 shown in fig2 and fig5 is then inserted in a forming machine such as a hydroform drawing or like machine which forms the bonded blank 30 by drawing the round blank 30 into a finished fry pan 70 , for example , having the round cookware shape as shown in fig7 . other composite bonded blank shapes , e . g ., oval , square , rectangular , may be used depending on the finished shape of the cookware desired . of course , it is well - known in bonding sheets of materials or blanks of materials to clean each layer of the material surfaces prior to bonding . this may be done in various known ways , such as in a protective atmosphere or by a cleaning technique whereas the oils are burned off , or by abrading the surface by grit blasting , or by wire abrasion , or by chemical activation and so on . in any event , the discs for bonding the composite blanks usually are in the form of a round shape ( or other desired shape ) of sufficient diameter to provide for a blank size which will permit , after bonding , the forming of a shape of the cookware of sufficient diameter to provide the cookware of the desired diameter with minimal or no scrap loss . in this manner , the present invention provides for a much more economical process for making near net sized bonded composite blanks wherein there is very little loss for scrap , particularly when considering the value of a composite material . conventionally , when wider strips of material are roll - bonded together , such as stainless steel , aluminum , copper , and stainless steel , into a roll - bonded strip and then blanked , the outlying materials forming a carrier web surrounding the blank are lost as scrap . this web material has much less value from a scrap standpoint because the web layers have been previously bonded together by rolling . to the contrary , in the present invention , only the round ( or other shape ) blank of material is formed as a composite bonded blank . as a result , there is no residual scrap composite material along the carrier web as in the prior conventional roll - bonding processing technique using continuous pre - bonded , composite strip materials . fig6 depicts the bonded layer 2 of stainless steel peeled from the underlying layer 4 of aluminum showing the undersides of several of the bubbles 20 . in actual tests , the undersides of the bubbles 20 are of lighter color , indicating no or lesser bonding between the first layer 2 of stainless steel and the aluminum layer 4 in the areas of the bubbles 20 compared to the flat areas therebetween . it is also important to note that in the present invention with the dimpled or bubble formation 20 being formed in the stacked array , that the dimpled or bubble configuration cannot be formed by conventional roll bonding . the aluminum material , being much more ductile than the stainless steel material , would not withstand the rolling forces so as to produce any dimpled effect in roll bonding . the aluminum would simply deform in a linear fashion and would not produce the required dimpled or bubble pattern finish in the stainless steel . it will be also understood that while the invention has been described as bonding only three materials together to form one composite blank 30 , the process could be easily adapted to bond more than a single composite blank . thus , a perforated plate ( if used ) could be positioned between the stacked arrays of blanks 30 to produce additional blanks of composite material which can be subsequently drawn into finished pans . this is likewise true of stacks of materials without the use of the perforated plate to merely bond stacks of composite blanks of a variety of materials together which can be then drawn directly into finished cookware without the waste of scrap material previously generated in conventional roll bonding . in this alternate embodiment , a solid disk 40 of , for example , stainless steel ( without perforations ) could be positioned between the adjacent stacked arrays of blanks to prevent bonding between the adjacent stacked arrays of blanks during application of pressure and heat , see fig8 . various flat discs , such as stainless steel , aluminum , copper and titanium in various combinations , could be used in bonding the near net shape composite blanks in stacked arrays . in practice , we have found that the use of a pressure fixture or jig 50 of fig8 is useful in applying an axial clamping pressure to the one or more stacked arrays of discs for bonding the composite blanks . the fixture comprises two opposed heavy round platens or plates 52 for engaging the respective upper and lower discs in the stacked array ( s ) of blank assemblies 30 . a plurality of heavy duty bolts 54 are fitted in holes spaced around the periphery of the platens . the bolts have headed portions 60 at one end and opposed threaded ends 56 to receive nuts 58 which , when tightened , force the platens together so as to apply a force in an axial direction , normal to the discs of the stacked array ( s ) of blank assemblies 30 situated between the opposed platens 52 . each of the blank assemblies 30 have a solid disc 40 of stainless steel or the like placed therebetween to prevent bonding between the adjacent blank assemblies 30 . in one present embodiment , ten bolts 54 are used to apply the bonding pressure . double nuts 58 may be used at each bolt end to ensure proper strength . after the desired clamping pressure is obtained , the fixture and stacked array ( s ) of blanks are moved to a furnace and heated in a normal atmosphere containing oxygen , to a desired temperature to achieve the bonding between the individual discs in the stack array ( s ) of each blank assembly 30 . alternatively , the stacked array of the blanks may be heated by an induction heating unit which is positioned adjacent to and around the stacked array of blanks so as to avoid heating the fixture 50 to high temperatures as would otherwise occur in a furnace . as mentioned above , in the event more than one multi - layered stacked arrays 30 of discs are to be bonded , a stainless steel disc 40 is inserted between adjacent stacked arrays to prevent bonding between adjacent stacked arrays of blanks . in one actual bonding test run three hundred blank assemblies 30 were constructed using three layers of round discs ( 14 ″ in diameter ) of stainless steel , aluminum , and stainless steel layers for each blank assembly 30 . the three hundred blank assemblies 30 were stacked in the pressure fixture 50 between the platens 52 . in this example , the fixture 50 measured about six feet in height and the steel platens 52 measured about one foot thick . the heavy platens minimize flexing in the platens to provide an even distribution of pressure across the stacks of blank assemblies 30 so as to achieve uniform bonding of the stainless steel - aluminum - stainless steel layers of each blank assembly . in this example , the fixture 50 had ten high - strength bolts 54 positioned evenly around the periphery of the round platens 52 . after the bolts 54 were tightened and a desired pressure of about 20 , 000 psi was achieved , the fixture 50 was placed in a furnace and heated to a temperature of about 860 ° f . to achieve excellent bonding throughout each of the three hundred stacked arrays of blank assemblies 30 . the economics of this method of making bonded composite blanks of a desired net shape ( diameter ) ready for forming is apparent . in the elevated temperature bonding step , it is not necessary to control the atmosphere in that a normal oxygen containing atmosphere is acceptable . also , it is preferred to surround the stack of preformed blanks with an induction heating means to heat only the blanks and not the fixture . in this manner , the fixture is not affected by the heat supplied by the induction heating means . while specific embodiments of the invention have been described in detail , it will be appreciated by those skilled in the art that various modifications and alternatives to those details could be developed in light of the overall teachings of the disclosure . the presently preferred embodiments described herein are meant to be illustrative only and not limiting as to the scope of the invention which is to be given the full breadth of the appended claims and any and all equivalents thereof .