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 » Piloting
Site Map Home Register Authors List Search Today's Posts Mark Forums Read Web Partners

V-n Diagrams



 
 
Thread Tools Display Modes
  #1  
Old August 29th 04, 04:38 PM
john smith
external usenet poster
 
Posts: n/a
Default

Greg Esres wrote:
I am using Vs (stall, clean) since the configuration is the same as
at Va.

Vs1 is normally taken to be the clean stall speed. The meaning of Vs
seems a bit more ambiguous. But we're talking the same thing here.

How does CAS account for density altitude?

With a given CAS, the density altitude is irrelevant. That's the
beauty of it. ;-)

For a given DA, you could use TAS and get the same results, as long as
you're consistent in using TAS for each figure. However, Vs1 is only
published as CAS. And there's no point in doing that anyway.


Thanks, Greg.
The whole purpose of my exercise is to determine the minimum turn radius
and maximum rate of turn for a given weight. This is dependent upon air
density (hence, density altitude) and true airspeed.
What is really interesting to me is, I learned all this stuff 25 years
ago, but didn't have the experience to fully understand it as I do now.

  #2  
Old August 30th 04, 05:58 AM
Greg Esres
external usenet poster
 
Posts: n/a
Default

The whole purpose of my exercise is to determine the minimum turn
radius and maximum rate of turn for a given weight. This is dependent
upon air density (hence, density altitude) and true airspeed.

Hmmm. Air density doesn't appear in the formulas that I have. Load
factor and true airspeed are the only variables. And load factor
should be independent of density altitude.

What are you doing with air density?
  #3  
Old August 30th 04, 02:48 PM
Jay Smith
external usenet poster
 
Posts: n/a
Default

Greg Esres wrote:
The whole purpose of my exercise is to determine the minimum turn
radius and maximum rate of turn for a given weight. This is dependent
upon air density (hence, density altitude) and true airspeed.


Hmmm. Air density doesn't appear in the formulas that I have. Load
factor and true airspeed are the only variables. And load factor
should be independent of density altitude.
What are you doing with air density?


Trying to figure minimum safe altitudes for recovery from vertical dives
at different times of the year under different temperature/humidity
conditions.

 




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
Maximum Sustained Turn Rate? Emilio Military Aviation 5 May 11th 04 03:12 AM
Piper Cheyenne wiring diagrams. Steve Piloting 1 April 7th 04 03:50 AM
FS: Aviation History Books Neil Cournoyer Military Aviation 0 August 26th 03 08:32 PM


All times are GMT +1. The time now is 09:35 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.