Challenge

FINAL INDEPENDENT PROJECT

FINAL INDEPENDENT PROJECT

TITLE:-F-16 AIRCRAFT DESIGN :-

OBJECTIVE:-

  • Design and modelling of components of F-16 JET, using sketch tools and 3D modelling features of Solidworks.
  • Assembly of car using Solidworks assembly tool.
  • Rendering images of car in Photoview360 and Solidworks visualization with different environments and views.

SPECIFICATION FOR F-16 JET:-

The F-16 is a single-engine fighter aircraft. It has a fuselage length of about 15 meters and a wingspan of about nine meters. The American fighter jet has an empty weight of 9,000 kilograms and reaches a top speed of Mach 2, or about 2,100 kilometers per hour.

Technical data:

F-16 FIGHTING FALCON

Length: 14,80 meters
Height: 4,8 meters
Maximum take-off weight:

16.875 kilogram

Maximum speed: 2.414 km/h
Flight altitude: 15.000 meters
Wing span:

9,8 meters

Design methodology –

Description –

3D modelling is the process of developing a representation of anything, it could be a real world thing like thing like – Sci-fi missiles, drones etc. 3D modelling has many types but for this we used surface modelling and solid modelling. In this project we used solid modelling features to model part of car and used surface modelling features to give shape to vehicle body and later we converted into solid body to give some extrudes and cuts. Journey starts with blueprint setup and ends with rendering.

The following parts are modelled –

1)FRONT WHEELS:-

BACK WHEELS:-

ENGINE:-

PILOT SEAT:-

MISSILES:-

VERTICAL TAIL:-

HORIZONATAL TAIL :-

WING:-

FUSELAG:-

COCKPIT:-

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