"Mathematical Methods in Aerodynamics" is a specialized book that focuses on the mathematical models and methods in aerodynamics. It provides a comprehensive analysis of the fundamental principles that govern the fluid mechanics of aircraft wings. The book discusses the historical developments in this field, starting with the groundbreaking work of L. Prandtl in 1918, who developed the first mathematical model for the study of aircraft wings. Readers gain insights into the integral equations used to calculate lift and moment coefficients, as well as the various hypotheses that describe the flow around wings. By combining theoretical foundations with practical applications, this book serves as a valuable reference for students and professionals engaged in aerodynamics and related disciplines.