Calculate V-speeds (Vr, V2, Vstall), best rate of climb (Vy), service ceiling, and range from aircraft performance parameters.
| Constant | Symbol | Value |
|---|---|---|
| Speed of light | c | 2.99792458×10⁸ |
| Planck's constant | h | 6.62607015×10⁻³‴ |
| Boltzmann constant | kʙ | 1.380649×10⁻²³ |
| Avogadro's number | Nₐ | 6.02214076×10²³ |
| Gravitational constant | G | 6.6743×10⁻¹¹ |
| Gas constant | R | 8.31446 |
| Elementary charge | e | 1.602176634×10⁻¹⁹ |
| Electron mass | mₑ | 9.1093837015×10⁻³¹ |
| Proton mass | mₚ | 1.67262192369×10⁻²⁷ |
| Fine-structure constant | α | 7.2973525693×10⁻³ |
The Aircraft Performance Calculator — V-speeds, Climb Rate & Range works by applying a well-defined formula to the values you enter. Understanding the formula behind the calculation helps you interpret the result and check that your inputs are correct. Below we break down the key components that drive the Aircraft Performance.
The core formula used by this calculator is:
Result = f(load, geometry, material, safety factor)
Each variable in the formula has a specific meaning:
Note: Engineering results must be checked against the applicable code (ISO, ASTM, ACI, NIST, etc.) and tolerances.