This textbook and its six supporting computer programs provide
theoretical modelling of the aerodynamic characteristics of wings and
bodies at low Mach numbers. The approach presented helps engineering
students improve problem-solving skills by discerning the necessary
steps associated with solving analytical problems. The book also
presents a justification and rationale for validating end results that
leave the student with an understanding of the answer and allow them to
determine the effects of modifying parameters and geometry.