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[v0.1]Space Shuttle Vanguard


NovaSilisko

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This is a common misconception, even among pilots, but it\'s totally untrue. A stalled wing still produces lift, just not as much as at a lower angle of attack.

Here\'s two graphs of wind tunnel measurements of lift vs. AoA for the same airfoil. The first is for normal (unstalled) conditions:

pre-stall.png

A stall happens when the aircraft\'s AoA exceeds that for maximum lift, which for this airfoil is between 12 and 15 degrees. Notice how the lift doesn\'t drop to zero beyond that point.

That graph only had data up to twenty degrees AoA. Here\'s what happens if you keep increasing the AoA:

post-stall.png

The lift doesn\'t reach zero until the AoA is past 90 degrees—that is, the wing has to be nearly flat to the oncoming wind to produce no lift!

The first graph is from Abbott & von Doenhoff, 1949, the second is from NASA CR-2008-215434.

You\'re correct. Let me rephrase, a stalled wing does not produce enough lift than what is necessary to keep the plane 'in the air'.

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I\'ve just performed a successful suborbital flight with vanguard. To perform a successful reentry, set your periapsis to 30,000m, and when you enter the atmosphere, orient yourself to the ground, and turn on SAS. Do NOT attempt to manuever at speeds above 200 m/s, it usually ends badly.

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Nova: Interesting discovery on my end working on the shuttle;

Angular Drag is the bread and butter of winglets more is better for stabilizing things. Try something like 20 and see if it still tries to flip out on launch.

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Guest GroundHOG-2010

your not doing the X37. Could I do a plane as a direct copy of the X37, since there isn\'t a direct copy of a real life planned spaceplane.

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