## Wave Drag Coefficient for Supersonic flow over a Flat Plate

The drag coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water …

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# aerospace calculator

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Wave Drag Coefficient for Supersonic flow over a Flat Plate

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Lift Coefficient for Supersonic flow over a Flat Plate

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Specific Heat at Constant Pressure

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Drag Coefficient of finite wing

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Oswald Efficiency Factor for Straight Wing

The drag coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water …

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Wave Drag Coefficient for Supersonic flow over a Flat Plate

The lift coefficient (CL) is a dimensionless coefficient that relates the lift generated by a lifting body to the fluid density around the body, the fluid velocity and an associated reference area. A lifting body is a foil or a…

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Lift Coefficient for Supersonic flow over a Flat Plate

Specific Heat for an Ideal Gas at Constant Pressure and Volume. This represents the dimensionless heat capacity at constant volume; it is generally a function of temperature due to intermolecular forces

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Specific Heat at Constant Pressure

the drag coefficient is a dimensionless quantity that is used to quantify the drag or resistance of an object in a fluid environment, such as air or water

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Drag Coefficient of finite wing

It is a correction factor that represents the change in drag with a lift of a three-dimensional wing or aeroplane, as compared with an ideal wing having the same aspect…

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Oswald Efficiency Factor for Straight Wing