Performance Analysis of Plug Nozzles for Turbojet and Rocket Exhausts
Keyword(s):
An attractive feature of the plug-type nozzle for turbojets and rocket jets is that it can automatically adjust its effective exit area with operating pressure ratio and achieve a high level of efficiency over a wide range of operating pressure ratio without variation of mechanical shape. The design and off-design performance analysis of such nozzles is described.
Keyword(s):
2020 ◽
Keyword(s):
1970 ◽
Vol 19
(1-2)
◽
pp. 264-267
◽
Keyword(s):
2021 ◽
Vol 18
(14)
◽
pp. 7480