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Description |
Relative suitability of the turboshaft (left), low bypass turbofans (middle) and ordinary turbojects (right) for the flight at the 10 km attitude in various speeds |
Source |
own drawing, used different information from K.Honicke, R.Lindner, P.Anders, M.Krahl, H.Hadrich, K.Rohricht. Beschreibung der Konstruktion der Triebwerksanlagen. Interflug, Berlin, 1968 for the data of this chart. |
Date |
Audriusa 21:15, 11 August 2006 (UTC) |
Author |
Audrius Meskauskas |
Permission |
GFDL |
Other versions |
JetSuitability.png (unlabelled) |
I, the author of this work, hereby publish it under the following license:
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Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.2 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the license is included in the section entitled " GNU Free Documentation License".
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