Simplified procedure has been developed to aid in reduction of data obtained by tailpipe or nozzle instrumentation; equations are derived from which working curves may be plotted to show clearly effect of changes in any variable; these curves are especially useful in flight test data reduction.
Determination of turbojet engine thrust from tailpipe measurements
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 14 , n 10
1947
4 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Aircraft turbojet engine comprising two thrust reverser modules
European Patent Office | 2023
|Optimizing Thrust Reversal for a Small Turbojet Engine
AIAA | 2024
|Turbojet engine nacelle comprising a thrust reverser drive mechanism
European Patent Office | 2020
|TURBOJET ENGINE NACELLE COMPRISING A THRUST REVERSER DRIVE MECHANISM
European Patent Office | 2018
|