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The NACA 5-series tool can be used to plot and extract coordinates of any NACA 5-series airfoil.
The NACA 5-series tool can be used to plot and extract coordinates of any NACA 5-series airfoil.
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28 September 2022
An aircraft electrical system includes an engine driven generator which provides a continuous source of electricity once the engine is running.
An aircraft electrical system includes an engine driven generator which provides a continuous source of electricity once the engine is running.
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28 September 2022
All aircraft are subjected to four fundamental forces in flight that governs their motion through the air: LIFT, WEIGHT, THRUST and DRAG.
All aircraft are subjected to four fundamental forces in flight that governs their motion through the air: LIFT, WEIGHT, THRUST and DRAG.
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18 May 2022
Learn more about an aircraft’s tail section with a focus on the tail’s impact in three primary areas: stability, control, and trim.
Learn more about an aircraft’s tail section with a focus on the tail’s impact in three primary areas: stability, control, and trim.
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18 May 2022
This post details the pitot static system which provides pressure readings to the three pressure-based primary flight instruments: the airspeed indicator, the altimeter, and the vertical speed indicator.
This post details the pitot static system which provides pressure readings to the three pressure-based primary flight instruments: the airspeed indicator, the altimeter, and the vertical speed indicator.
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28 September 2022
The reference wing area is defined as the plan area of an aircraft's wing.
The reference wing area is defined as the plan area of an aircraft's wing.
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19 May 2022
An interactive carburetor icing calculator designed to assist pilots in identifying the typical conditions where carburetor icing is most likely to occur.
An interactive carburetor icing calculator designed to assist pilots in identifying the typical conditions where carburetor icing is most likely to occur.
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27 July 2023
The variation in turbulent flat plate skin friction coefficient with Reynolds number is used when compiling an estimation of aircraft parasitic drag.
The variation in turbulent flat plate skin friction coefficient with Reynolds number is used when compiling an estimation of aircraft parasitic drag.
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28 September 2020
Angle of attack refers to the angle between a reference line on a body and the vector representing the relative motion between the body and the fluid through which it is moving.
Angle of attack refers to the angle between a reference line on a body and the vector representing the relative motion between the body and the fluid through which it is moving.
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19 May 2022
This calculator provides an estimation of the interference factor between a wing and a fuselage and is used when estimating aircraft parasitic drag.
This calculator provides an estimation of the interference factor between a wing and a fuselage and is used when estimating aircraft parasitic drag.
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28 September 2020
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