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This report provides data for preliminary and detailed design of wing, fuselage, control surface and landing gear of a 120 seated passenger aircraft with the knowledge of design data from previous design project. In this, the theoretical aspect of aerodynamics, aircraft structure, propulsion, stability and control are given as per the need for desi...
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The design optimisation of aerostructures is largely based on Multidisciplinary Design Optimisation (MDO), which is a set of tools used by the aircraft industry to size primary structures: wings, large portions of the fuselage or even an entire aircraft. The procedure is computationally expensive, as it must account for several thousands of loadcas...
Citations
The VTOL aircrafts are also considered the next generation aircrafts which can land on any terrain. These aircrafts are considered to be the next generation which won't require a long runway to land and takeoff. Blended wing is the design in which wings are integrated into the fuselage which reduces the drag increasing the fuel efficiency of the aircraft. These two features can provide an aircraft which can also be used for military purposes in cross-border troop transport and bombing runs without getting detected in the enemy radar. This paper gives an idea of a conceptual design of such an aircraft. Few of the parameters of the aircraft based on the weight requirements for the desired mission (Bombing runs) is taken which is usually high as the aircraft should be able to carry enough bombs than the current bombers with greater fuel efficiency.
