GATE 2017-2018 :: GATE Aeronautical Engineering
- The constraint A2 = A on any square matrix A is satisfied for
- The general solution of the different equation d2y/dt2 + dy/dt - 2t = 0 is
- An aircraft in trimmed condition has zero pitching moment at
- In an aircraft, constant roll rate can be produced using ailerons by applying
- For a symmetric airfoil, the lift coefficient for zero degree angle of attack is
- The critical Mach number of an airfoil is attained when
- The shadowgraph flow visualization technique depends on
- The Hohmann ellipse used as earth-Mars transfer orbit has
- The governing equation for the static transverse deflection of a beam under an uniformly distributed load, according to Euler-Bernoulli (engineering) beam theory, is a
- The Poisson's ratio,ν of most aircraft grade metallic alloys has values in the range:
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