Open AccessEffect of Convergent Section Contour on the Sonic Line in Rocket Engine Nozzles
Author(s) -
Eduardo Matos Germer,
Carlos Henrique Marchi
Publication year - 2018
Publication title -
journal of aerospace technology and management
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.265
H-Index - 19
eISSN - 2175-9146
pISSN - 1984-9648
DOI - 10.5028/jatm.v10.924
Subject(s) - rocket engine , nozzle , rocket (weapon) , section (typography) , aerospace engineering , line (geometry) , rocket engine nozzle , aero engine , contour line , engineering , aeronautics , acoustics , materials science , mechanical engineering , physics , computer science , geometry , meteorology , mathematics , operating system
Accelerating Research
Robert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom
Address
John Eccles HouseRobert Robinson Avenue,
Oxford Science Park, Oxford
OX4 4GP, United Kingdom