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On a typical aerofoil, a point exists about which the resultant aerodynamic pitching moment M is independent of incidence. This special point is called the Aerodynamic Centre (AC).
minimum mass of air required for complete combustionof the HFO
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Lifting wing FP was run at the conditions corresponding to AGARD WG07 TEST CASE 11, namely M∞ = 0.84,α= 3.06 deg. The ‘final step' values of the partially-conservative paramete
a note on tracing a closed loop. What are the characteristic features of a closed loop?(
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Q. Explain the following with reference to deformation of metals: (1) Preferred orientation (2) Elastic after effect
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apply equations to solve problems for specified aerodynamic applications. Need some inputs regarding this.
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