Composite are occupying the place of conventional materials by meeting the requirements of industries of not only in aerospace sector but in automotive, mechanical, space, construction industries and Bio medical applications, but the desire of achieving the higher modulus to density ratio always remains starved as it requires the maximum output in minimal consumption with better life expectancy to find the economical means of utilizing the technology for different applications. In need of which researches have been emerged to obtain the hybrid composites by the combination of multiple types of materials to obtain the desired strength with less density. For most of the applications of Automotive, Aerospace and biomedical applications, the flexural strength plays a crucial role as the structure continuously or repeatedly subjects to point or uniform load, therefore a study to evaluate the flexural strength by using different types of matrix material and also to optimize the thickness of lamina is done, and comparisons are made by using different categories of matrix material on different thickness of laminates.