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Aspect Ratio Calculator Wing

Aspect Ratio Formula:

\[ AR = \frac{wing\_span^2}{wing\_area} \]

meters
square meters

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1. What is Wing Aspect Ratio?

Definition: The aspect ratio of a wing is the ratio of its span to its mean chord, or equivalently, the square of the span divided by the wing area.

Purpose: It's a key parameter in aircraft design that affects aerodynamic efficiency, lift distribution, and structural weight.

2. How Does the Calculator Work?

The calculator uses the formula:

\[ AR = \frac{wing\_span^2}{wing\_area} \]

Where:

Explanation: Higher aspect ratios indicate longer, narrower wings which are more efficient for cruising but may compromise maneuverability.

3. Importance of Aspect Ratio

Details: Aspect ratio significantly impacts:

4. Using the Calculator

Tips: Enter the wing span in meters and wing area in square meters. Both values must be > 0.

5. Frequently Asked Questions (FAQ)

Q1: What's a typical aspect ratio for commercial airliners?
A: Commercial jets typically have aspect ratios between 7:1 and 10:1 for optimal cruise efficiency.

Q2: What about gliders or high-performance sailplanes?
A: Gliders often have much higher aspect ratios (20:1 to 30:1) for maximum lift with minimal drag.

Q3: How does aspect ratio affect aircraft performance?
A: Higher AR generally means less induced drag but more structural weight and reduced maneuverability.

Q4: What's the aspect ratio of fighter jets?
A: Fighter aircraft typically have low aspect ratios (3:1 to 5:1) for high maneuverability and structural strength.

Q5: Can I calculate AR if I know wing chord instead of area?
A: Yes, for rectangular wings, AR = span/chord. For tapered wings, use the mean aerodynamic chord.

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