Necessity of designing tail pipe burners with low burner inlet velocity, low burner drag, and high diffuser efficiency in order to obtain both high thrust augmentation and to minimize loss in normal engine performance during nonburning operation is illustrated.
Theoretical analysis of various thrust-augmentation cycles for turbojet engines
Nat Advisory Committee Aeronautics -- Tech Note
1950
52 pages
Diagrams, Charts
Report
English
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Theoretical analysis of various thrust-augmentation cycles for turbojet engines
Engineering Index Backfile | 1950
|Theoretical comparison of several methods of thrust augmentation for turbojet engines
Engineering Index Backfile | 1950
|