:[EMAIL PROTECTED] On Behalf Of J Hudson
Sent: Wednesday, 31 January 2007 1:13 PM
To: Discussion of issues relating to Soaring in Australia.
Subject: Re: [Aus-soaring] Manometer Construction
I am seeking info on the manometer scale above 160 Kts for ASI Calibration,
up to say 250 Kts.
Basic Sailplane
: [EMAIL PROTECTED]
[mailto:[EMAIL PROTECTED] On Behalf Of J Hudson
Sent: Wednesday, 31 January 2007 1:13 PM
To: Discussion of issues relating to Soaring in Australia.
Subject: Re: [Aus-soaring] Manometer Construction
I am seeking info on the manometer scale above 160 Kts for ASI
Calibration,
up to say
At 05:52 PM 31/01/2007, you wrote:
Good work Ken.. Reminds me of the time you worked out that a Ka6
could not fly above 96,000 feet because the Vne equaled the stalling
speed.. good memories from 40 years ago. :)
I suspect the limiting mach number would make it somewhat les than 96000
4. If you lowered the nose do descend you would bust vne.
i think several X aircraft were lost due to this .. i could be wrong.
Ben
- Original Message -
From: Graham Watts [EMAIL PROTECTED]
Subject: Re: [Aus-soaring] Manometer Construction
Good work Ken.. Reminds me
As I understand it the U2 flew pretty close to coffin corner all the
time
Dave O
On 31/01/2007, at 8:34 PM, Ben Jones wrote:
Isn't that condition called by jet jockies as Coffin Corner
1. If you increased hight you would bust vne and prob fall apart ,
2. If you stalled recovering the
-To: Discussion of issues relating to Soaring in
Australia.aus-soaring@lists.internode.on.net
To: Discussion of issues relating to Soaring in
Australia.aus-soaring@lists.internode.on.net
Subject: Re: [Aus-soaring] Manometer Construction
Date: Wed, 31 Jan 2007 19:34:43 +0900
Isn't that condition called by jet
On Wed, 2007-01-31 at 19:19 +1000, Mike Borgelt wrote:
At 05:52 PM 31/01/2007, you wrote:
Good work Ken.. Reminds me of the time you worked out that a Ka6
could not fly above 96,000 feet because the Vne equaled the stalling
speed.. good memories from 40 years ago. :)
I suspect the
At 10:31 PM 31/01/2007, you wrote:
On Wed, 2007-01-31 at 19:19 +1000, Mike Borgelt wrote:
At 05:52 PM 31/01/2007, you wrote:
Good work Ken.. Reminds me of the time you worked out that a Ka6
could not fly above 96,000 feet because the Vne equaled the stalling
speed.. good memories from 40
I am seeking info on the manometer scale above 160 Kts for ASI Calibration,
up to say 250 Kts.
Basic Sailplane Engineering provides the info up to 160 Kts.
Ive been unable to locate any info - and the scale to 160 Kts does not
appear consistent, let alone to 250 Kts.
Thanks in anticipation,
On Wed, 2007-01-31 at 12:43 +1030, J Hudson wrote:
I am seeking info on the manometer scale above 160 Kts for ASI Calibration,
up to say 250 Kts.
Basic Sailplane Engineering provides the info up to 160 Kts.
Ive been unable to locate any info - and the scale to 160 Kts does not
appear
Good work Ken.. Reminds me of the time you worked out that a Ka6 could
not fly above 96,000 feet because the Vne equaled the stalling speed..
good memories from 40 years ago. :)
Ken Caldwell wrote:
On Wed, 2007-01-31 at 12:43 +1030, J Hudson wrote:
I am seeking info on the manometer
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