AE2258 AERODYNAMICS LAB SYLLABUS | ANNA UNIVERSITY BE AERONAUTICAL ENGINEERING 4TH SEM SYLLABUS REGULATION 2008 2011 2012-2013 BELOW IS THE ANNA UNIVERSITY FOURTH SEMESTER BE AERONAUTICAL ENGINEERING DEPARTMENT SYLLABUS, TEXTBOOKS, REFERENCE BOOKS,EXAM PORTIONS,QUESTION BANK,PREVIOUS YEAR QUESTION PAPERS,MODEL QUESTION PAPERS, CLASS NOTES, IMPORTANT 2 MARKS, 8 MARKS, 16 MARKS TOPICS. 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
AE2257 AIRCRAFT STRUCTURES LAB –I L T P C
0 0 3 2
OBJECTIVE
To study experimentally the load deflection characteristics structural materials under
different types of loads.
LIST OF EXPERIMENTS
1. Determination of Young’s modulus of steel using mechanical extensometers.
2. Determination of Young’s modulus of aluminum using electrical extensometers
3. Determination of fracture strength and fracture pattern of ductile and brittle
materials
4. Determination of forces in statically indeterminate force system.
5. Deflection of beams with various end conditions.
6. Verification of Maxwell’s Reciprocal theorem & principle of superposition
7. Column – Testing
8. South – well’s plot.
9. Testing of Riveted Joints.
10. Determination of membrane stresses in a thin cylinder under internal pressure.
TOTAL: 45 PERIODS
LIST OF EQUIPMENTS
(for a batch of 30 students)
Sl. No. Equipments Qty Experiments No.
1. Universal Testing Machine 1 1,2,3, 9
2. Mechanical Extensometer 1 1
3. Electrical strain gauge 10 2, 4, 10
4. Hinged bar suspended by two wires of
different materials. 1 4
5. Strain indicator 1 2, 4, 10
6. Dial Gauges 12 5, 6
7. Beam Test set up with various end
conditions 2 5, 6
8. Column Test Apparatus 1 7, 8
9. Thin walled pressure vessel 1 10
39
AE2258 AERODYNAMICS LABORATORY L T P C
0 0 3 2
OBJECTIVE
To familiarize the students in basic aerodynamics and use of wind tunnels.
LIST OF EXPERIMENTS
1. Generation of lift and tip vortices.
2. Flow visualization in water flow channel
3. Flow visualization in smoke tunnel
4. Plot of RPM Vs test section velocity in a subsonic wind tunnel.
5. Pressure distribution over circular cylinder.
6. Pressure distribution over airfoil and estimation of CL and CD.
7. Force measurement using wind tunnel balance.
8. Mach number distribution in nozzle of supersonic wind tunnel.
9. Use of Schlieren system to visualize shock.
10. Use of Shadow graph system to visualize shock.
TOTAL: 45 PERIODS
LIST OF EQUIPMENT
(for a batch of 30 students)
Sl.
No.
Items Quantity Experiment
No.
1. Blower, Balance, and small aspect ratio model 1 each. 1
2. Water flow channel & models 1 set 2
3. Subsonic wind tunnel 1 No. 3, 4,5,6,7
4. Smoke apparatus and rake 1 each. 3
5. Manometer, Pitot-Static tube 1 No. 4,5,6
6. Circular cylinder and Aerofoil pressure distribution
models
1 each 5,6
7. Wind tunnel strain gauge balance 1 No. 7
8. Supersonic wind tunnel, Mercury manometer 1 No. 8,9,10
9. Schlieren system and Shadow graph system 1 No. 9,10
10. Sharp nosed and Blunt nosed models 1 No.
each
9,10
AE2257 AIRCRAFT STRUCTURES LAB –I L T P C
0 0 3 2
OBJECTIVE
To study experimentally the load deflection characteristics structural materials under
different types of loads.
LIST OF EXPERIMENTS
1. Determination of Young’s modulus of steel using mechanical extensometers.
2. Determination of Young’s modulus of aluminum using electrical extensometers
3. Determination of fracture strength and fracture pattern of ductile and brittle
materials
4. Determination of forces in statically indeterminate force system.
5. Deflection of beams with various end conditions.
6. Verification of Maxwell’s Reciprocal theorem & principle of superposition
7. Column – Testing
8. South – well’s plot.
9. Testing of Riveted Joints.
10. Determination of membrane stresses in a thin cylinder under internal pressure.
TOTAL: 45 PERIODS
LIST OF EQUIPMENTS
(for a batch of 30 students)
Sl. No. Equipments Qty Experiments No.
1. Universal Testing Machine 1 1,2,3, 9
2. Mechanical Extensometer 1 1
3. Electrical strain gauge 10 2, 4, 10
4. Hinged bar suspended by two wires of
different materials. 1 4
5. Strain indicator 1 2, 4, 10
6. Dial Gauges 12 5, 6
7. Beam Test set up with various end
conditions 2 5, 6
8. Column Test Apparatus 1 7, 8
9. Thin walled pressure vessel 1 10
39
AE2258 AERODYNAMICS LABORATORY L T P C
0 0 3 2
OBJECTIVE
To familiarize the students in basic aerodynamics and use of wind tunnels.
LIST OF EXPERIMENTS
1. Generation of lift and tip vortices.
2. Flow visualization in water flow channel
3. Flow visualization in smoke tunnel
4. Plot of RPM Vs test section velocity in a subsonic wind tunnel.
5. Pressure distribution over circular cylinder.
6. Pressure distribution over airfoil and estimation of CL and CD.
7. Force measurement using wind tunnel balance.
8. Mach number distribution in nozzle of supersonic wind tunnel.
9. Use of Schlieren system to visualize shock.
10. Use of Shadow graph system to visualize shock.
TOTAL: 45 PERIODS
LIST OF EQUIPMENT
(for a batch of 30 students)
Sl.
No.
Items Quantity Experiment
No.
1. Blower, Balance, and small aspect ratio model 1 each. 1
2. Water flow channel & models 1 set 2
3. Subsonic wind tunnel 1 No. 3, 4,5,6,7
4. Smoke apparatus and rake 1 each. 3
5. Manometer, Pitot-Static tube 1 No. 4,5,6
6. Circular cylinder and Aerofoil pressure distribution
models
1 each 5,6
7. Wind tunnel strain gauge balance 1 No. 7
8. Supersonic wind tunnel, Mercury manometer 1 No. 8,9,10
9. Schlieren system and Shadow graph system 1 No. 9,10
10. Sharp nosed and Blunt nosed models 1 No.
each
9,10
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