<?xml version="1.0" encoding="UTF-8"?><rss version="2.0"
	xmlns:content="http://purl.org/rss/1.0/modules/content/"
	xmlns:dc="http://purl.org/dc/elements/1.1/"
	xmlns:atom="http://www.w3.org/2005/Atom"
	xmlns:sy="http://purl.org/rss/1.0/modules/syndication/"
		>
<channel>
	<title>Comments on: Tail boom strakes</title>
	<atom:link href="http://blog.aopa.org/helicopter/?feed=rss2&#038;p=309" rel="self" type="application/rss+xml" />
	<link>http://blog.aopa.org/helicopter/?p=309</link>
	<description>AOPA's Helicopter Blog</description>
	<lastBuildDate>Wed, 19 Jun 2013 15:56:57 +0000</lastBuildDate>
	<sy:updatePeriod>hourly</sy:updatePeriod>
	<sy:updateFrequency>1</sy:updateFrequency>
	<generator>http://wordpress.org/?v=3.5.1</generator>
	<item>
		<title>By: Ken Armstrong</title>
		<link>http://blog.aopa.org/helicopter/?p=309#comment-978</link>
		<dc:creator>Ken Armstrong</dc:creator>
		<pubDate>Fri, 23 Apr 2010 14:50:17 +0000</pubDate>
		<guid isPermaLink="false">http://blog.aopa.org/helicopter/?p=309#comment-978</guid>
		<description><![CDATA[Tim,
It might be better to point out the strake is effective because it is installed such that it trips the air on the side on which is installed making a low pressure area along the tail boom (and obviously high pressure on the other side).  This force helps the tail rotor in the hover by reducing the amount of anti-torque it needs to provide and allows the altitude and payload increases.

The NASA team used wind tunnel and
flight test data to design a device that improves
handling qualities, reduces tailboom fatigue, improves
climb and cruise performance, and increases
yaw control safety margins for all single
rotor helicopters with enclosed tailbooms.
http://www.blrvgs.com/pdfs/techbrief.pdf

Happy hover landings

Ken]]></description>
		<content:encoded><![CDATA[<p>Tim,<br />
It might be better to point out the strake is effective because it is installed such that it trips the air on the side on which is installed making a low pressure area along the tail boom (and obviously high pressure on the other side).  This force helps the tail rotor in the hover by reducing the amount of anti-torque it needs to provide and allows the altitude and payload increases.</p>
<p>The NASA team used wind tunnel and<br />
flight test data to design a device that improves<br />
handling qualities, reduces tailboom fatigue, improves<br />
climb and cruise performance, and increases<br />
yaw control safety margins for all single<br />
rotor helicopters with enclosed tailbooms.<br />
<a href="http://www.blrvgs.com/pdfs/techbrief.pdf" rel="nofollow">http://www.blrvgs.com/pdfs/techbrief.pdf</a></p>
<p>Happy hover landings</p>
<p>Ken</p>
]]></content:encoded>
	</item>
	<item>
		<title>By: Brendan Fitzpatrick</title>
		<link>http://blog.aopa.org/helicopter/?p=309#comment-976</link>
		<dc:creator>Brendan Fitzpatrick</dc:creator>
		<pubDate>Fri, 23 Apr 2010 14:02:06 +0000</pubDate>
		<guid isPermaLink="false">http://blog.aopa.org/helicopter/?p=309#comment-976</guid>
		<description><![CDATA[Good stuff!  Thanks Tim.]]></description>
		<content:encoded><![CDATA[<p>Good stuff!  Thanks Tim.</p>
]]></content:encoded>
	</item>
</channel>
</rss>
