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Numbers in a glide

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Old 30th May 2018 | 11:07
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Numbers in a glide

Hi!
Some questions that are appearing in performance exams compare a light and a hevier aircraft in a glide.

So, I know the heavy aircraft will have an increased ROD. But what about the descent gradient and angle?

Descent gradient is proportional to ROD (Gradient = ROD/TAS * 6000/6080). So, gradient will also increase?

And what about descent angle? If Gradient = tan(angle) * 100, will this also increase?

Thanks!
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Old 30th May 2018 | 11:21
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The still air descent angle in a glide depends upon the lift/drag ratio.

To maintain the optimum glide angle at a higher weight will require a higher speed.

The glide angle will not change.

For teaching purposes I drew a diagram to illustrate this. If I can dig it out I will post it.
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Old 30th May 2018 | 11:32
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There's something i'm missing here.

If you increase speed in a glide (decreasing your AOA), how can your glide angle not change?

Thanks!!
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Old 30th May 2018 | 16:12
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If you increase speed in a glide (decreasing your AOA), how can your glide angle not change?
The point is that you don't decrease your angle of attack.

The higher weight means that you will achieve a higher speed at the same angle of attack, maintaining the best L/D ratio as before.
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Old 30th May 2018 | 18:39
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From: in a 5 m/s thermal
Look up a glide polar, on that, you can see, that the polar slides on the line which is tangent to the optimum speed point. Therefore, as described above, the speed of max L/D increases (as well as the associated vertical speed, however, the ratio stays the same).

(altough, sometimes the actual glide ratio can vary on gliders with the ballast, especially on the longer ones, as with water on board the wing is more stiff, helping to stay at the optimal shape at high speed, more likely with older designs)

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Old 31st May 2018 | 06:30
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Ok, so the speed will increase and so the ROD, but gradient and and angle will be constant, it's this correct?

Thank you all for your help!
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Old 31st May 2018 | 07:09
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From: in a 5 m/s thermal
Imagine it as a triangle.
On the first one, your forward speed is 50 m/s, and the vertical speed is 2 m/s.
You are heavier, therefore the optimum is say, 100m/s, the correspodning vertical speed is 4m/s. So the ratio is still 25:1(you will land at the same spot, altough you will get there faster), and as both sides of the triangle enlarge by the same factor, the angle should be the same. So the angle will be the same, and the gradient is the same as the glide ratio (expressed in other values) so yes, they will be the same.

Hope its getting clearer.
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Old 31st May 2018 | 07:41
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The triangle explanation is perfect, now I get it. Thanks hoduka!!
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