Augmented Vectored Thrust Engines and the Problem of Avoiding Hot Gas Recirculation

1980 ◽  
Vol 102 (1) ◽  
pp. 61-67 ◽  
Author(s):  
W. J. Lewis ◽  
R. Hurd

It can be argued that the vectored thrust engine is one of the best propulsion systems for V/STOL combat aircraft. The next step is to consider the problems to be overcome in integrating such a powerplant into the airframe. A critical installation issue, and one which is not unique to vectored thrust systems, is that of hot exhaust gas recirculation. In this paper some of Rolls-Royce’s hot gas recirculation experience is described, covering, in particular, the creation of a specialized recirculation test facility and some sample test results. The application of the results to a vectored thrust installation is discussed, together with some of the implications for the aircraft designer. Finally, some comments are made regarding the requirements of other V/STOL propulsion systems to avoid excessive hot gas recirculation.

2010 ◽  
Vol 141 (2) ◽  
pp. 74-81
Author(s):  
Marek RUDKOWSKI ◽  
Sławomir DUDEK ◽  
Ryszard WOŁOSZYN

The paper presents results of research designed and constructed by the authors of external exhaust gas recirculation Integral Engine-Compressor Cooper Bessemer GMVH-8. This system was used primarily to reduce emissions of nitrogen oxides


Fuel ◽  
2021 ◽  
Vol 303 ◽  
pp. 121297
Author(s):  
A. Zachl ◽  
M. Buchmayr ◽  
J. Gruber ◽  
A. Anca-Couce ◽  
R. Scharler ◽  
...  

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