Billede:JetSuitabilityEn.png

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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:
GNU head 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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