A aviation & planes forum. AviationBanter

If this is your first visit, be sure to check out the FAQ by clicking the link above. You may have to register before you can post: click the register link above to proceed. To start viewing messages, select the forum that you want to visit from the selection below.

Go Back   Home » AviationBanter forum » rec.aviation newsgroups » Soaring
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

What's your favorite youtube speedpass?



 
 
Thread Tools Display Modes
Prev Previous Post   Next Post Next
  #10  
Old January 23rd 14, 06:22 PM posted to rec.aviation.soaring
Bob Whelan[_3_]
external usenet poster
 
Posts: 400
Default What's your favorite youtube speedpass?

On 1/23/2014 7:18 AM, kirk.stant wrote (w. some snippage):


http://www.youtube.com/watch?v=2S7T81LbvIs


Nice pass!

A question for all you aero majors out the when pulling up at high
speed, should you lead with the flaps, or follow with them?

In this vid, pilot pulls, then lowers flaps after speed has dropped. My
understanding is that it is more efficient to lower flaps (from cruise to
zero, then positive as you slow) during the pull, and my experience
somewhat bears that out (higher alt gain with a good pull and simultaneous
flaps).


Neither lead nor follow?

Here's an attempt at one of those potentially worthless - in the sense that
for all practical purposes it can be neither effectively measured nor
implemented in real time - responses that might just shed some theoretical
light upon one's flying techniques...

If we - for the purposes of a pullup - define "efficiency" as "least
aerodynamic drag possible per time instant" (since both drag and gravity
oppose the ship's ability to trade kinetic energy for height) then the answer
to the question obviously (!) is the flaps should be placed in whatever
position minimizes aerodynamic drag for that instant's speed...think polar.

Complicating factors almost certainly include time and flap position, since
for any given (ever-increasing) amount of flap deflection (below the
separation angle of attack) the wing section can generate greater total lift,
which for a fixed-weight condition will be proportional to "wing developable
G." So, will a shorter time at high G (and drag) - meaning a shorter time to
change pitch angle from (say) "descending through pitched up" - result in
greater speed at the start of the ascent than a "theoretically most
aerodynamically efficient (longer-in-time) configuration" through the same
angular change?

I don't know, but my suspicion is aerodynamic efficiency would trump. In any
event, if we take "the rapid pitch-up" scenario to an extreme, various
fighters can demonstrate that a rapid pitch-up is a great way to bleed energy
and speed (think "the cobra maneuver").

As foe Joe Glider Pilot, this is a great example of one (ideally, many)
test(s) being worth ten thousand considered opinions! Kids, don't do this test
in the pattern...

Bob - it's still winter... - W.
 




Thread Tools
Display Modes

Posting Rules
You may not post new threads
You may not post replies
You may not post attachments
You may not edit your posts

vB code is On
Smilies are On
[IMG] code is On
HTML code is Off
Forum Jump

Similar Threads
Thread Thread Starter Forum Replies Last Post
My favorite nice guy Aviation Photos 0 October 20th 09 11:29 AM
Favorite Airlines Kloudy via AviationKB.com Piloting 0 May 7th 08 06:20 PM
Favorite picture of my favorite airplane. russell[_2_] Aviation Photos 3 August 4th 07 04:39 PM
Your favorite altitude Mxsmanic Piloting 87 May 4th 07 09:53 PM
Which one's my favorite cheese? Michael Baldwin, Bruce Products 5 January 20th 07 04:07 PM


All times are GMT +1. The time now is 09:14 PM.


Powered by vBulletin® Version 3.6.4
Copyright ©2000 - 2025, Jelsoft Enterprises Ltd.
Copyright ©2004-2025 AviationBanter.
The comments are property of their posters.