Aircraft Structures I AE2254 ND2012 Question Paper

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Anna University Question Paper Code : 11023
BE / B.Tech EXAMINATION, NOVEMBER/DECEMBER 2012. 
Fourth Semester 
Aeronautical Engineering 
AE2264/111404/AN 45/A1 1263/10122 AE 405/080180014 AIRCRAFT STRUCTURES I
(Regulation 2008) 

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PART A — (10 x2 = 20 marks)

1, Explain the method of joints used fir the plane truss analysis.
2. Explain the difference in the stress distribution between beam made of one materiel and compositor beam.
3. Explain Clapeyron'e three moment theorem used for the analysis of continuous hes, M.
4, Define stiffness factor, distribution factor and carry over factor..
6. Write down the, expression for strain energy stored for axial loading, bending and shear. Pi, Explain the unit load method.
7. Write down the expressions for critical buckling load for column with ends fixed, ends hinged, one end fixed and the other end free and one end fixed and the other end hinged in the seconding order of buckling load.
8. Briefly explain the use of Rankine'it formula.
9 Explain the use of Southwell plot.
10. State the maximum stress theory and maximum shear stress theory.

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