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Aerodynamic force and Thrust

Shortcuts: Differences, Similarities, Jaccard Similarity Coefficient, References.

Difference between Aerodynamic force and Thrust

Aerodynamic force vs. Thrust

The aerodynamic force is the force exerted on a body by the air (or some other gas) in which the body is immersed, and is due to the relative motion between the body and the gas. Thrust is a reaction force described quantitatively by Newton's third law.

Similarities between Aerodynamic force and Thrust

Aerodynamic force and Thrust have 4 things in common (in Unionpedia): Drag (physics), Euclidean vector, Jet engine, Propeller (aeronautics).

Drag (physics)

In fluid dynamics, drag (sometimes called air resistance, a type of friction, or fluid resistance, another type of friction or fluid friction) is a force acting opposite to the relative motion of any object moving with respect to a surrounding fluid.

Aerodynamic force and Drag (physics) · Drag (physics) and Thrust · See more »

Euclidean vector

In mathematics, physics, and engineering, a Euclidean vector (sometimes called a geometric or spatial vector, or—as here—simply a vector) is a geometric object that has magnitude (or length) and direction.

Aerodynamic force and Euclidean vector · Euclidean vector and Thrust · See more »

Jet engine

A jet engine is a type of reaction engine discharging a fast-moving jet that generates thrust by jet propulsion.

Aerodynamic force and Jet engine · Jet engine and Thrust · See more »

Propeller (aeronautics)

An aircraft propeller, or airscrew,Beaumont, R.A.; Aeronautical Engineering, Odhams, 1942, Chapter 13, "Airscrews".

Aerodynamic force and Propeller (aeronautics) · Propeller (aeronautics) and Thrust · See more »

The list above answers the following questions

Aerodynamic force and Thrust Comparison

Aerodynamic force has 21 relations, while Thrust has 48. As they have in common 4, the Jaccard index is 5.80% = 4 / (21 + 48).

References

This article shows the relationship between Aerodynamic force and Thrust. To access each article from which the information was extracted, please visit:

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