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Thursday, February 5, 2009
AIRCRAFT STRUCTURES-I
Assignment No: 1
1. Derive the Clapeyron’s three moment equation (16).
2. What is strain energy? (2)
3. Define Cantigliano’s theorem (2).
4. Define Maxwell’s Reciprocal theorem.(2)
5. Explain Eccentric loading? (2)
6. Explain Euler’s column curve. (2)
7. Derive Maximum Shear Stress theory (16).
8. What is Composite beam? (2)
9. Define Johnson’s parabolic formula. (2)
10. Define Rankine’s formula. (2)
Submit the above on the re-opening day .
1. Derive the Clapeyron’s three moment equation (16).
2. What is strain energy? (2)
3. Define Cantigliano’s theorem (2).
4. Define Maxwell’s Reciprocal theorem.(2)
5. Explain Eccentric loading? (2)
6. Explain Euler’s column curve. (2)
7. Derive Maximum Shear Stress theory (16).
8. What is Composite beam? (2)
9. Define Johnson’s parabolic formula. (2)
10. Define Rankine’s formula. (2)
Submit the above on the re-opening day .
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