AE2404 AIRCRAFT DESIGN PROJECT – II SYLLABUS | ANNA UNIVERSITY BE AERONAUTICAL 7TH SEM SYLLABUS REGULATION 2008 2011 2012-2013 BELOW IS THE ANNA UNIVERSITY SEVENTH SEMESTER BE AERONAUTICAL ENGINEERING DEPARTMENT SYLLABUS, TEXTBOOKS, REFERENCE BOOKS,EXAM PORTIONS IT IS APPLICABLE FOR ALL STUDENTS ADMITTED IN THE YEAR 2011 2012-2013 (ANNA UNIVERSITY CHENNAI,TRICHY,MADURAI,TIRUNELVELI,COIMBATORE), 2008 REGULATION OF ANNA UNIVERSITY CHENNAI AND STUDENTS ADMITTED IN ANNA UNIVERSITY CHENNAI DURING 2009
AE2404 AIRCRAFT DESIGN PROJECT – II L T P C
0 0 3 2
OBJECTIVE
To enhance the knowledge in continuation of the design given in project–I
Each student is assigned the work in continuation of the design project – I. The
following assignments are to be carried out.
LIST OF EXPERIMENTS
1. V-n diagram for the design study
2. Gust and maneuverability envelopes
3. Critical loading performance and final V-n graph calculation
4. Structural design study – Theory approach
5. Load estimation of wings
6. Load estimation of fuselage.
7. Balancing and Maneuvering loads on tail plane, Aileron and Rudder loads.
8. Detailed structural layouts
9. Design of some components of wings, fuselage
10. Preparation of a detailed design report with drawings.
TOTAL: 45 PERIODS
66
LIST OF EQUIPMENTS
(for a batch of 30 students)
S.No. Items Quantity
1. Drawing Board 30
2. Drawing Instrument 20
3. Computers and suitable
software
30
AE2404 AIRCRAFT DESIGN PROJECT – II L T P C
0 0 3 2
OBJECTIVE
To enhance the knowledge in continuation of the design given in project–I
Each student is assigned the work in continuation of the design project – I. The
following assignments are to be carried out.
LIST OF EXPERIMENTS
1. V-n diagram for the design study
2. Gust and maneuverability envelopes
3. Critical loading performance and final V-n graph calculation
4. Structural design study – Theory approach
5. Load estimation of wings
6. Load estimation of fuselage.
7. Balancing and Maneuvering loads on tail plane, Aileron and Rudder loads.
8. Detailed structural layouts
9. Design of some components of wings, fuselage
10. Preparation of a detailed design report with drawings.
TOTAL: 45 PERIODS
66
LIST OF EQUIPMENTS
(for a batch of 30 students)
S.No. Items Quantity
1. Drawing Board 30
2. Drawing Instrument 20
3. Computers and suitable
software
30
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