Free Online Practice mock Test 1 for GATE 2016 Aeronautical engineering. GATE syllabus and Previous Year Question Papers with Answers Free Download.

1. The constraint A^{2} = A on any square matrix A is satisfied for
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2. The general solution of the different equation d^{2}y/dt^{2} + dy/dt - 2t = 0 is
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3. An aircraft in trimmed condition has zero pitching moment at
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4. In an aircraft, constant roll rate can be produced using ailerons by applying
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5. For a symmetric airfoil, the lift coefficient for zero degree angle of attack is
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