Flow over idealized nozzle computed. Analysis and computer program calculate flow over idealized mixer nozzle. Nozzle idealized by unwrapping it so planform lies in z=O plane. Linearized compresible flow used to calculate flow and mixer shape given loading on mixer. End goal to achieve maximum amount of mixing downstream of mixer while retaining reasonable shape for mixer. Because analysis assumes linearized flow, calculation of effects of deep lobe penetration cannot be made using this program.
Mixer Analysis of Nacelle/Nozzle Flow
NASA Tech Briefs ; 10 , 2
1986-06-01
Miscellaneous
No indication
English
NACELLE FOR AN AIRCRAFT ENGINE WITH VARIABLE SECTION NOZZLE
European Patent Office | 2016
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