Aircraft Design detail syllabus for Aeronautical Engineering (Aero), 2017 regulation is taken from Anna University official website and presented for students of Anna University. The details of the course are: course code (AE8604), Category (PC), Contact Periods/week (3), Teaching hours/week (3), Practical Hours/week (0). The total course credits are given in combined syllabus.
For all other aero 6th sem syllabus for be 2017 regulation anna univ you can visit Aero 6th Sem syllabus for BE 2017 regulation Anna Univ Subjects. The detail syllabus for aircraft design is as follows.”
Course Objective:
- To make the student understand the choice of the selection of design parameters, Fixing the geometry and to investigate the performance and stability characteristics of airplanes.
Unit I
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Unit II
Preliminary Design Procedure
Data collection and 3-view drawings/ their purpose, weight estimation, Weight equation method -Development and procedures for evaluation of component weights. Weight fractions for various segments of mission. Choice of wind loading and thrust. Loading .
Unit III
Power Plant Selection
Choices available, comparative merits, Location of power plants, Functions dictating the locations.
Unit IV
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Unit V
Design of Landing Gear and Control Surface
Landing Gear Design, Loads on landing gear, Preliminary landing gear design. Elements of Computer Aided and Design, Special consideration in configuration lay-out, Performance estimation.Stability aspects on the design of control surface.
Course Outcome:
Students will be able to
- Initiate the preliminary design of an aircraft starting from data collection to satisfy mission specifications;
- To get familiarized with the estimation of geometric and design parameters of an airplane
- Understanding the procedure involved in weight estimation, power plant selection, estimation of the performance parameters, stability aspects, design of structural components of the airplane, stability of structural elements, estimation of critical loads etc.
- Initiate the design of a system, component, or process to meet requirements for aircraft systems;
- Complete the design of an aircraft to a level of sufficient detail to demonstrate that it satisfies given mission specifications
- Work in a multidisciplinary environment involving the integration of engineering practices in such subjects as aerodynamics, structures, propulsion, and flight mechanics
Text Books:
- Raymer, D.P. Aircraft conceptual Design, AIAA series, 5th edition, 2012.
- Torenbeck, E. Synthesis of Subsonic Airplane Design, Delft University Press, U.K. 1986.
References:
- Kuechemann, D, The Aerodynamic Design of Aircraft, American Institute of Aeronautics publishers, 2012
For detail syllabus of all other subjects of BE Aero, 2017 regulation do visit Aero 6th Sem syllabus for 2017 Regulation.
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