Aircraft Design Project – II for B.Tech 7th sem is covered here. This gives the details about credits, number of hours and other details along with reference books for the course.
The detailed syllabus for Aircraft Design Project – II B.Tech (R13) seventhsem is as follows.
OBJECTIVES:
- Each group of students is assigned to continue the structural design part of the airplane. The following are the assignments are to be carried out.
- Preliminary design of an aircraft wing – Shrenck’s curve, structural load distribution, shear force, bending moment and torque diagrams
- Detailed design of an aircraft wing – Design of spars and stringers, bending stress and shear flow calculations – buckling analysis of wing panels
- Preliminary design of an aircraft fuselage – load distribution on an aircraft fuselage
- Detailed design of an aircraft fuselage – design of bulkheads and longerons – bending stress and shear flow calculations – buckling analysis of fuselage panels
- Design of control surfaces – balancing and maneuvering loads on the tail plane and aileron, rudder loads
- Design of wing-root attachment
- Landing gear design
- Preparation of a detailed design report with CAD drawings
TOTAL: 45 PERIODS
OUTCOMES:
- On completion of Aircraft design project II the students will be in a position to design aircraft wings, fuselage, loading gears etc., and also able to angle the design in terms of structural point of view.
For all other B.Tech AE 7th sem syllabus go to Anna University B.Tech AERONAUTICAL ENGINEERING (AE) 7th Sem Course Structure for (R13) Batch.All details and yearly new syllabus will be updated here time to time. Subscribe, like us on facebook and follow us on google plus for all updates.
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