Aerodynamic Design of Transport Aircraft by E. Obert

By E. Obert

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Another example of this is the horizontal tail of the F-16, it was designed to have sufficient stability but had a lack of manoeuvrability Extra when performing highly dynamic manoeuvres. When performing these highly dynamic manoeuvres or “jinking” the horizontal tail stalled. 5. 5 - Horizontal tail of the F-16 5. Filling the “empty shell” Once the aerodynamic shape is determined detail design is performed on: t Cabin and cockpit arrangement t All aircraft systems t Aircraft structure This is where the more abstract results from the previous parts of the aircraft design process are converted into hardware.

13 AERODYNAMIC DESIGN OF TRANSPORT AIRCRAFT Examples of wrong specification Dassault Mercure: Instead of designing the aircraft for a maximum range, Dassault chose to design the Mercure for the average range demanded by airlines. This range was only a fourth of the maximum range, resulting in a design that was not flexible in range and consequently it was an economic failure. 1 - Dassault Mercure. Source: Andrew Hunt VFW 614: This aircraft was technically too complicated for the intended market section at its time of introduction and therefore not affordable.

Numbers and types of existing aircraft and their condition) The economic situation (What is the economic growth projection? Who has the money? What is the tariff structure? ) Knowledge and insight is required of performance aerodynamics, the achievable engine performance and all weight aspects. The development of the Boeing 747 shows how important weight is. The first ideas were that 350 passengers could be transported over 5100 nm at a MTOW of 550,000 lb. The increase in weight during the development had a “snowball effect”, a small increase in weight of some component resulted in a further increase in total weight and so on.

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