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<div class="moz-cite-prefix">On 01/12/2020 21:11, Herrell, Dave
wrote:<br>
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<p><snip> ( emphasis in extracted text is my own - OM):<br>
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<blockquote type="cite"
cite="mid:fbf3f4874ab243b4bef39c23261e31e9@mpr.com">
<pre class="moz-quote-pre" wrap=""> This new location and larger size of nacelle cause the vortex flow off the nacelle body to produce lift at high AoA. As the nacelle is ahead of the C of G, this lift <b>causes a slight pitch-up effect</b> (ie a reducing stick force) which could lead the pilot to inadvertently pull the yoke further aft than intended bringing the aircraft closer towards the stall. </pre>
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<p>I had actually read this text on the web before Dave quoted it
here ... and yet PBL has said in a previous posting:</p>
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<p>>>>As far as I am aware, there is no "pitch-up tendency
[which] starts to lift the aircraft's nose". <br>
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<p>These positions appear to me to contradict each other.<br>
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<p>Two questions:</p>
<p>1. Who is right? PBL or the Boeing people who produced the text
that Dave Herrell quoted?</p>
<p>2. If the forces on the stick change rapidly, this suggests, to
me at least, that the aerodynamic pressure on the relevant control
surfaces (thinking physics again) changes rapidly at some point,
hence the question, what causes the sudden change of pressure?
Flow separation from the HS, possibly??<br>
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<p>And if PBL whinges again about repeating himself, I would
respectfully remind him that</p>
<p>(1) Repeating oneself and expressing oneself clearly are two
different things.</p>
<p>(2) Repeatedly asking people to say clearly what they mean is a
foul habit that I acquired by reading about the cantankerous
ancient Greek criminal, Socrates.<br>
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<p>Still confused,</p>
<p>Olwen</p>
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