The Downwash Angle Calculator determines the angle at which the airflow is deflected downward behind a wing due to lift generation. It is a crucial parameter in aerodynamics, affecting aircraft de stabilité, efficiency, and induced drag. This calculator helps engineers, pilots, and aviation enthusiasts estimate the downwash angle based on clé aerodynamic properties of the wing.
Formula of Downwash Angle Calculator
Downwash Angle (ε) is calculated as:
Downwash Angle (ε) = (2 × CL) / (π × AR × e)
Où :
- ε is the downwash angle in radians
- CL is the lift coefficient of the wing
- AR is the aspect ratio of the wing (wingspan²/wing area)
- π est d'environ 3.14159
- e is the wing efficiency factor (typically 0.7-0.95 depending on wing planform)
This formula helps estimate the induced flux angle behind a lifting surface, which impacts aircraft performance.
Precomputed Values for Quick Reference
The following table provides approximate downwash angles for common wing configurations:
| Type d'aile | Coefficient de portance (CL) | Rapport hauteur/largeur (AR) | Efficiency Factor (e) | Downwash Angle (ε) (radians) |
|---|---|---|---|---|
| Low-Aspect Jet Wing | 0.5 | 6 | 0.8 | 0.053 |
| High-Aspect Glider Wing | 0.7 | 12 | 0.9 | 0.041 |
| Commercial Airliner Wing | 0.6 | 9 | 0.85 | 0.049 |
| Fighter Jet Wing | 0.8 | 4 | 0.75 | 0.085 |
This table allows users to quickly estimate downwash angles without manually calculating them.
Example of Downwash Angle Calculator
Suppose an aircraft wing has the following properties:
- Coefficient de portance (CL) = 0.6
- Rapport hauteur/largeur (AR) = 8
- Wing Efficiency Factor (e) = 0.85
En utilisant la formule :
ε = (2 × 0.6) / (π × 8 × 0.85) ε ≈ 1.2 / (3.14159 × 6.8) ε ≈ 1.2 / 21.36 ε ≈ 0.0562 radians
Converting to degrees:
ε ≈ 0.0562 × (180/π) ε ≈ 3.22°
This means that the downwash angle for this specific wing configuration is about Degrés 3.22.
FAQ les plus courantes
The downwash angle affects induced drag and aircraft stability. A higher downwash angle increases drag and impacts efficiency.
A higher aspect ratio reduces the downwash angle, leading to better aerodynamic efficiency and lower induced drag.
The wing efficiency factor usually ranges from 0.7 (for low-efficiency wings) to 0.95 (for high-efficiency wings like gliders).