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The velocity at a point on the wing placed in a wind tunnel is \(251 m/s\). The pressure and temperature …
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Find the coefficient of pressure at a point on the wing where the velocity is \(58\,m/s\). The airplane is flying …
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Calculate the pressure coefficient at a point on the airfoil where the pressure is \( 8.9 \times 10^4\,N/m^2\). Airfoil is …
- 11 views
- 1 answers
- 0 votes
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Calculate the lift, drag and moment coefficient about quarter chord per unit span of an airfoil which is at an …
- 18 views
- 1 answers
- 0 votes
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What are angle of attack, absolute angle of attack and induced angle of attack ?
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What is center of pressure and aerodynamic center ?
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Why induced drag is minimum for an elliptical wing planform ?
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What are neutral point and static margin of an aircraft ?
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- 1 answers
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What are longitudinal static stability, directional static stability and lateral static stability for an airplane ?
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What is the difference between symmetrical and asymmetrical /cambered airfoil ?
- 48 views
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Find the coefficient of pressure at a point on the wing.
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Calculate the pressure coefficient at a point on the airfoil.
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Angle of attack, Absolute angle of attack and Induced angle of attack
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