document.write( "Question 426518: Engineers use complex mathematical formulas when designing aircrafts. For example, stringers used in the wing of an air plane must be able to support a certain load. Engineers have to use a stringer with the right diameter for the job. Using a smaller size poses a safety hazard. Using a larger size is a waste of material and will result in increased cost to the plane's operator.\r
\n" );
document.write( "\n" );
document.write( "Let's assume that the stress S on a rod is given by the formula,\r
\n" );
document.write( "\n" );
document.write( "S = (load)/(cross sectional area).\r
\n" );
document.write( "\n" );
document.write( "Let's assume that the air plane uses an aluminium rod with diameter 20mm to support a load of 5 x 10^4 Newton. Engineers know that maximum stress on Aluminium is 1 x 10^ 8 Newtons/m^2. How do we determine whether the rod can withstand the load?
\n" );
document.write( "
\n" );
document.write( " \n" );
document.write( "
Algebra.Com's Answer #296694 by htmentor(1343) You can put this solution on YOUR website! The cross sectional area of a rod = \n" ); document.write( "Therefore A = \n" ); document.write( "Convert the area to square meters: 314.16 mm^2*(1 m/1000 mm)^2 = 3.1416 x 10^-4 \n" ); document.write( "We are given S = 1 x 10^8, and L = 5 x 10^4 \n" ); document.write( "For the rod to withstand the load, we need the stress to be less than 1 x 10^8 \n" ); document.write( "Since S = L/A, we have S = 5 x 10^4/3.1416 x 10^-4 = 1.59 x 10^8 N/m^2. \n" ); document.write( "This value is greater than the maximum stress of 1 x 10^8, so the rod will not withstand the load. \n" ); document.write( " |