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BE/BTech  Aeronautical Aircraft Structures Define: Plasticity ellipse.
BE/BTech  Aeronautical Aircraft Structures Define : Octahedral Stresses
BE/BTech  Aeronautical Aircraft Structures Write the failure theories and its relationship between tension and shear.
BE/BTech  Aeronautical Aircraft Structures Write the limitations of Maximum Strain Energy Theory. ( Beltrami Theory).
BE/BTech  Aeronautical Aircraft Structures Write the limitations of Maximum Shear Strain Theory.(Von –Mises Hencky theory orDistortion energy theory).
BE/BTech  Aeronautical Aircraft Structures Write the limitations of Maximum Shear Stress Theory. ( Tresca’ s theory).
BE/BTech  Aeronautical Aircraft Structures Write the limitations of Maximum Principal Stress Theory. (Rakine’ s theory)
BE/BTech  Aeronautical Aircraft Structures What are the theories used for ductile failures?
BE/BTech  Aeronautical Aircraft Structures Define: Maximum Strain Energy Theory (Beltrami Theory)
BE/BTech  Aeronautical Aircraft Structures Define : Maximum Shear Strain Theory (Von –Mises Hencky theory or Distortion energytheory)
BE/BTech  Aeronautical Aircraft Structures Define : Maximum Shear Stress Theory. ( Tresca’ s theory)
BE/BTech  Aeronautical Aircraft Structures Define: Maximum Principal Strain Theory. ( St. Venant’ s theory)
BE/BTech  Aeronautical Aircraft Structures Define: Maximum Principal Stress Theory. (Rakine’ s theory)
BE/BTech  Aeronautical Aircraft Structures List out different theories of failure
BE/BTech  Aeronautical Aircraft Structures What are the types of failures?
BE/BTech  Aeronautical Aircraft Structures Write the general expressions for the maximum bending moment, if the deflection curveequation is given.
BE/BTech  Aeronautical Aircraft Structures Write the expressions for the deflection developed in a beam column carrying several pointloads at different distances with an axial load, hinged at both ends.
BE/BTech  Aeronautical Aircraft Structures Write the expressions for the maximum bending moment and max, stress developed in a beamcolumn carrying uniformly distributed load with axial load, hinged at both ends.
BE/BTech  Aeronautical Aircraft Structures Write the expressions for the maximum deflection developed in a beam column carryinguniformly distributed load with axial load, hinged at both ends.
BE/BTech  Aeronautical Aircraft Structures Write the expressions for the maximum bending moment and max. stress developed in a beamcolumn carrying central point load hinged at both ends.
BE/BTech  Aeronautical Aircraft Structures Write the expressions for the maximum deflection developed in a beam column carrying centralpoint load with axial load, hinged at both ends.
BE/BTech  Aeronautical Aircraft Structures What is beam column? Give examples
BE/BTech  Aeronautical Aircraft Structures Write Euler’ s formula for maximum stress for a eccentrically loaded column?
BE/BTech  Aeronautical Aircraft Structures Write Euler’ s formula for maximum stress for a initially bent column?
BE/BTech  Aeronautical Aircraft Structures Give Rakine’ s formula and its advantages.
BE/BTech  Aeronautical Aircraft Structures What are the uses of south well plot? (column curve).
BE/BTech  Aeronautical Aircraft Structures Define: Equivalent length of the column
BE/BTech  Aeronautical Aircraft Structures Write the Euler’ s formula for different end conditions.
BE/BTech  Aeronautical Aircraft Structures What are the limitations of the Euler’ s formula?
BE/BTech  Aeronautical Aircraft Structures What are the assumptions followed in Euler’ s equation?
BE/BTech  Aeronautical Aircraft Structures Differentiate short and long column
BE/BTech  Aeronautical Aircraft Structures What are the factors affect the strength column?
BE/BTech  Aeronautical Aircraft Structures What is slenderness ratio ( buckling factor)? What is its relevance in column?
BE/BTech  Aeronautical Aircraft Structures What are the types of column failure?
BE/BTech  Aeronautical Aircraft Structures Define: Column
BE/BTech  Aeronautical Aircraft Structures Define : Trussed Beam.
BE/BTech  Aeronautical Aircraft Structures Define : Modulus of resilience.
BE/BTech  Aeronautical Aircraft Structures Compare the unit load method and Castigliano’ s first theorem
BE/BTech  Aeronautical Aircraft Structures Give the procedure for unit load method.
BE/BTech  Aeronautical Aircraft Structures Define: Unit load method.
BE/BTech  Aeronautical Aircraft Structures Define : Maxwell Reciprocal Theorem.
BE/BTech  Aeronautical Aircraft Structures What are uses of Castigliano’ s first theorem?
BE/BTech  Aeronautical Aircraft Structures Write the Castigliano’ s first theorem.
BE/BTech  Aeronautical Aircraft Structures Write down the formula to calculate the strain energy, if the applied tension load is given.
BE/BTech  Aeronautical Aircraft Structures Write down the formula to calculate the strain energy , if the torsion moment value is given.
BE/BTech  Aeronautical Aircraft Structures Write down the formula to calculate the strain energy , if the moment value is given
BE/BTech  Aeronautical Aircraft Structures Write down the formula to calculate the strain energy due to pure shear, if shear stress is given.
BE/BTech  Aeronautical Aircraft Structures Write the formula to calculate the strain energy due to pure shear
BE/BTech  Aeronautical Aircraft Structures Write the formula to calculate the strain energy due to torsion
BE/BTech  Aeronautical Aircraft Structures Write the formula to calculate the strain energy due to bending.
BE/BTech  Aeronautical Aircraft Structures Write the formula to calculate the strain energy due to axial loads ( tension).
BE/BTech  Aeronautical Aircraft Structures Define: Proof Resilience.
BE/BTech  Aeronautical Aircraft Structures Define: Strain Energy
BE/BTech  Aeronautical Aircraft Structures Write the two conditions for the analysis of composite beam.
BE/BTech  Aeronautical Aircraft Structures Define: Composite beam.
BE/BTech  Aeronautical Aircraft Structures Define: Constant strength beam.
BE/BTech  Aeronautical Aircraft Structures Define Flexural Rigidity of Beams.
BE/BTech  Aeronautical Aircraft Structures Define: Carry over moment and Carry over factor.
BE/BTech  Aeronautical Aircraft Structures Define: Distribution factor.
BE/BTech  Aeronautical Aircraft Structures Define: Stiffness factor.
BE/BTech  Aeronautical Aircraft Structures Define: Moment distribution method.( Hardy Cross mrthod).
BE/BTech  Aeronautical Aircraft Structures Give the procedure for analyzing the continuous beams with fixed ends using three momentequations?
BE/BTech  Aeronautical Aircraft Structures Write down the Clapeyron’s three moment equations for the continuous beam carrying UDL onboth the spans.
BE/BTech  Aeronautical Aircraft Structures Write down the Clapeyron’s three moment equations for the fixed beam
BE/BTech  Aeronautical Aircraft Structures Write down the Clapeyron’s three moment equations for the continuous beam with sinking at thesupports.
BE/BTech  Aeronautical Aircraft Structures Write down the general form of Clapeyron’s three moment equations for the continuous beam.
BE/BTech  Aeronautical Aircraft Structures What are the advantages of Continuous beam over simply supported beam?
BE/BTech  Aeronautical Aircraft Structures Define: Continuous beam.
BE/BTech  Aeronautical Aircraft Structures Differentiate the statically determinate structures and statically indeterminate structures?
BE/BTech  Aeronautical Aircraft Structures Explain with examples the statically indeterminate structures.
BE/BTech  Aeronautical Aircraft Structures What are the primary and secondary stresses in the analysis of a truss?
BE/BTech  Aeronautical Aircraft Structures A perfect frame consists of 7 members. Find the number of joints?
BE/BTech  Aeronautical Aircraft Structures Give relation between the numbers of members and joints in a truss and explain its uses?
BE/BTech  Aeronautical Aircraft Structures What are the hints to be followed while analyzing a simply supported truss using method ofjoints?
BE/BTech  Aeronautical Aircraft Structures What are the hints to be followed while analyzing a cantilever truss using method of joints?
BE/BTech  Aeronautical Aircraft Structures What is cantilever truss? What is simply supported truss?
BE/BTech  Aeronautical Aircraft Structures What are conditions of equilibrium used in the method of joints? Why?
BE/BTech  Aeronautical Aircraft Structures What are the assumptions made in the analyze of a truss?
BE/BTech  Aeronautical Aircraft Structures What are the methods used to analyze the plane & space frames?
BE/BTech  Aeronautical Aircraft Structures Define Plane truss and Space truss? Give some examples
BE/BTech  Aeronautical Aircraft Structures Differentiate the deficient frame and redundant frame?
BE/BTech  Aeronautical Aircraft Structures Differentiate the perfect and imperfect frames?
BE/BTech  Aeronautical Aircraft Structures What are the types of frames.
BE/BTech  Aeronautical Aircraft Structures Differentiate Truss and Frame?
BE/BTech  Aeronautical Aircraft Structures Explain with examples the statically determinate structures.
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