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Calculate lift, wave-drag and pressure coefficients of an infinitely thin flat plate which is in a Mach \(2.5\) freestream flow …
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- 1 answers
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What are form drag and profile drag ?
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- 1 answers
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A positively cambered airfoil has a zero-lift angle of \(-3.5^{\circ}\). The lift slope for this airfoil is \(0.12\) per degree. …
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- 1 answers
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Find the lift and wave drag coefficients for an infinitely thin flat plate at an angle of attack of \(8^{\circ}\) …
- 517 views
- 1 answers
- 0 votes
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Find the gliding distance of an aircraft flying at an altitude of \(1500\,m\) with a maximum lift to drag ratio …
- 632 views
- 1 answers
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Calculate the lift, drag and moment coefficient about quarter chord per unit span of an airfoil which is at an …
- 739 views
- 1 answers
- 0 votes
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What is flaps and what are they used for?
- 604 views
- 1 answers
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What is the difference between static and dynamic stability of an aircraft?
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- 1 answers
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Induced drag is minimum for which type of a wing planform
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- 4 answers
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What are profile drag, parasite drag, induced drag and wave drag?
- 867 views
- 1 answers
- 0 votes
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