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  2. Aerodynamic force - Wikipedia

    en.wikipedia.org/wiki/Aerodynamic_force

    The aerodynamic force is the resultant vector from adding the lift vector, perpendicular to the flow direction, and the drag vector, parallel to the flow direction. Forces on an aerofoil . In fluid mechanics , an aerodynamic force is a force exerted on a body by the air (or other gas ) in which the body is immersed, and is due to the relative ...

  3. Lift (force) - Wikipedia

    en.wikipedia.org/wiki/Lift_(force)

    The above lift equation neglects the skin friction forces, which are small compared to the pressure forces. By using the streamwise vector i parallel to the freestream in place of k in the integral, we obtain an expression for the pressure drag D p (which includes the pressure portion of the profile drag and, if the wing is three-dimensional ...

  4. Aerodynamics - Wikipedia

    en.wikipedia.org/wiki/Aerodynamics

    In many aerodynamics problems, the forces of interest are the fundamental forces of flight: lift, drag, thrust, and weight. Of these, lift and drag are aerodynamic forces, i.e. forces due to air flow over a solid body. Calculation of these quantities is often founded upon the assumption that the flow field behaves as a continuum.

  5. Drag (physics) - Wikipedia

    en.wikipedia.org/wiki/Drag_(physics)

    In aerodynamics, aerodynamic drag, also known as air resistance, is the fluid drag force that acts on any moving solid body in the direction of the air's freestream flow. [ 22 ] From the body's perspective (near-field approach), the drag results from forces due to pressure distributions over the body surface, symbolized D p r {\displaystyle D ...

  6. Stability derivatives - Wikipedia

    en.wikipedia.org/wiki/Stability_derivatives

    The aerodynamic forces are generated with respect to body axes, which is not an inertial frame. In order to calculate the motion, the forces must be referred to inertial axes. This requires the body components of velocity to be resolved through the heading angle ( β ) {\displaystyle (\beta )} into inertial axes.

  7. Fay-Riddell equation - Wikipedia

    en.wikipedia.org/wiki/Fay-Riddell_equation

    The Fay-Riddell equation is widely used in the design and analysis of thermal protection systems for re-entry vehicles. [ 3 ] [ 4 ] [ 5 ] It provides engineers with a crucial tool for estimating the severe aerodynamic heating conditions encountered during atmospheric entry and for designing appropriate thermal protection measures.

  8. Thrust - Wikipedia

    en.wikipedia.org/wiki/Thrust

    Thrust is a reaction force described quantitatively by Newton's third law. When a system expels or accelerates mass in one direction, the accelerated mass will cause a force of equal magnitude but opposite direction to be applied to that system. [2] The force applied on a surface in a direction perpendicular or normal to

  9. Strouhal number - Wikipedia

    en.wikipedia.org/wiki/Strouhal_number

    F = net external forces, L = characteristic length. This provides a dimensionless basis for a relationship between mass, characteristic speed, net external forces, and length (size) which can be used to analyze the effects of fluid mechanics on a body with mass. If the net external forces are predominantly elastic, we can use Hooke’s Law to see