The Reynolds number calculator can either be used in manual mode or alternatively used in with the standard atmosphere calculator.
A method of sizing an engine and propeller for a light sport aircraft is described and thrust curves plotted to determine maximum theoretical speed.
This standard atmosphere calculator is based on the 1976 model of the U.S. Standard Atmosphere.
The drag polar is a fundamental aspect of aircraft design and performance analysis. This tutorial will provide you with the tools to construct your own.
A post on the design of the horizontal and vertical tail, and an introduction to a method to size both surfaces.
An introduction to aircraft fuselage design. Construction methods, sizing, and fuselage loading.
This tutorial the Fundamentals of Aircraft Design series looks in more detail at sweep angle and why sweep is necessary for supersonic flight.
This tutorial focuses on wing area and aspect ratio and how these geometric variables drive an aircraft wing design.
An introduction to the aerodynamic lift, drag, and pitching moment coefficient with an example from two NACA airfoils.
An overview of all aspects associated with light aircraft propellers including forces, design, and how to manage a propeller in flight.
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