EFTA00848646.pdf
📄 Extracted Text (310 words)
From: "jeffrey E." <[email protected]>
To: lvjet
Subject:
Date: Sun, 16 Aug 2015 01:30:24 +0000
Up to about 28,000 feet the aircraft is limited by indicated air speed (Vne), so say you can do 350 kias at ground
level, you can do that all the way up to 28,000 too. Above that the limit is by Mach number (Mmo), as you
continue to climb your indicated air speed and your ground speed now decline as your Mach number remains
constant.
However, even though you are slowing down you engines are burning less and less fuel, part of this is from the
decreased IAS, but part is from the cold air. Colder air gives greater charge weight, it can be compressed more
and the engines get greater thermodynamic efficiency.
Eventually you reach the lowest clean IAS for your current weight, and that's as high as you are going. It doesn't
make any difference how much power you could add, you still can't climb because to do so you would need to
slow down or break up, and to slow down you'd have to start deploying high lift devices which increase drag and
reduce efficiency. This is what's called the coffin corner, your engines are probably running near max power, you
are near or at max speed and you are just above the stall.
please note
The information contained in this communication is
confidential, may be attorney-client privileged, may
constitute inside information, and is intended only for
the use of the addressee. It is the property of
JEE
Unauthorized use, disclosure or copying of this
communication or any part thereof is strictly prohibited
and may be unlawful. If you have received this
communication in error, please notify us immediately by
return e-mail or by e-mail to jeevacation®gmail.com, and
destroy this communication and all copies thereof,
including all attachments. copyright -all rights reserved
EFTA00848646
ℹ️ Document Details
SHA-256
25e483b08d489cb09e7a3eb1dadcbd5a742c16e6ec3265d755d49194f89214d7
Bates Number
EFTA00848646
Dataset
DataSet-9
Document Type
document
Pages
1
Comments 0