drag

pkg/drag

This package provides functionality for calculating the drag force on a rocket.

Responsibility

• Calculate the drag force on a rocket.
• Account for different drag coefficients based on the rocket's shape and velocity.
• Consider the effects of air density and viscosity.

Scope

• Support different drag models, such as the Newtonian drag model and the semi-empirical drag model.
• Provide options for customizing the drag calculation process.

Gotchas

• Accuracy of the drag coefficient data.
• Complexity of the drag models.

Test Suite Overview

The test suite includes unit tests for the core functionality of the package, including:

• Calculating the drag force on a rocket.
• Accounting for different drag coefficients.
• Considering the effects of air density and viscosity.