![]() The theoretical calculation of the airloads on the airplane is too large a subject to be covered in a structures book and It is customary in college aeronautical curricula to provide a separata course for this subject. Likewise, the fuselage or airplane body itself influences the airflow over the wing. are units that effect the airflow around the wing and thus effect the magnitude and distribution of the air forces on the wing. The presence of power plant nacelle units, external fuel tanks, etc. ![]() Furthermore, there is a wide range of wing configurations, such as the straight tapered wing, the swept wing and the delta wing, and many of these wings often include leading and trailing edge devices for promoting better lift or control characteristics. The complete determination of the air loads on an airplane requires a thorough theoretical knowledge of aerodynamics, since modern aircraft fly in sub-sonic, trans-sonic and super-sonic speed ranges. Before the structural design of an airplane can be made, the external loads acting on the airplane in flight, landing and take-off conditions must be known.
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