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	<title>Comments on: an airplane, flying in the direction of 40degree east of north at 475 mph in still air, encounter a 30-mph tai?</title>
	<atom:link href="http://airtim.es/airplane-flying/an-airplane-flying-in-the-direction-of-40degree-east-of-north-at-475-mph-in-still-air-encounter-a-30-mph-tai/feed" rel="self" type="application/rss+xml" />
	<link>http://airtim.es/airplane-flying/an-airplane-flying-in-the-direction-of-40degree-east-of-north-at-475-mph-in-still-air-encounter-a-30-mph-tai</link>
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		<title>By: Messiah's Mistress</title>
		<link>http://airtim.es/airplane-flying/an-airplane-flying-in-the-direction-of-40degree-east-of-north-at-475-mph-in-still-air-encounter-a-30-mph-tai/comment-page-1#comment-3640</link>
		<dc:creator>Messiah's Mistress</dc:creator>
		<pubDate>Wed, 04 Nov 2009 19:24:59 +0000</pubDate>
		<guid isPermaLink="false">http://airtim.es/airplane-flying/an-airplane-flying-in-the-direction-of-40degree-east-of-north-at-475-mph-in-still-air-encounter-a-30-mph-tai#comment-3640</guid>
		<description>http://www.youtube.com/watch?v=eBgLvN10ufA&amp;NR=1&lt;br&gt;&lt;b&gt;References : &lt;/b&gt;&lt;br&gt;</description>
		<content:encoded><![CDATA[<p><a href="http://www.youtube.com/watch?v=eBgLvN10ufA&amp;NR=1" rel="nofollow">http://www.youtube.com/watch?v=eBgLvN10ufA&amp;NR=1</a><br /><b>References : </b></p>
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		<title>By: M</title>
		<link>http://airtim.es/airplane-flying/an-airplane-flying-in-the-direction-of-40degree-east-of-north-at-475-mph-in-still-air-encounter-a-30-mph-tai/comment-page-1#comment-3639</link>
		<dc:creator>M</dc:creator>
		<pubDate>Wed, 04 Nov 2009 19:16:59 +0000</pubDate>
		<guid isPermaLink="false">http://airtim.es/airplane-flying/an-airplane-flying-in-the-direction-of-40degree-east-of-north-at-475-mph-in-still-air-encounter-a-30-mph-tai#comment-3639</guid>
		<description>V_g = V_a + V_w

V_g = speed over ground
V_a = airspeed
V_w = wind speed

V_a = V sin(40) i + V cos(40) j; V = 475 mph
V_w = - W sin(40) i + W cos(40) j; W = 30 mph

V_g = (V - W) sin(40) i + (V+W) cos(40) j = Vx i + Vy j

Speed = sqrt(Vx^2 + Vy^2)

Direction angle = 90 - atan(Vy/Vx)&lt;br&gt;&lt;b&gt;References : &lt;/b&gt;&lt;br&gt;</description>
		<content:encoded><![CDATA[<p>V_g = V_a + V_w</p>
<p>V_g = speed over ground<br />
V_a = airspeed<br />
V_w = wind speed</p>
<p>V_a = V sin(40) i + V cos(40) j; V = 475 mph<br />
V_w = &#8211; W sin(40) i + W cos(40) j; W = 30 mph</p>
<p>V_g = (V &#8211; W) sin(40) i + (V+W) cos(40) j = Vx i + Vy j</p>
<p>Speed = sqrt(Vx^2 + Vy^2)</p>
<p>Direction angle = 90 &#8211; atan(Vy/Vx)<br /><b>References : </b></p>
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