Investigation of transonic aerodynamic performance characteristics of six nozzles using hot jet exhaust provided by hydrogen peroxide system; 12-tube and 12-lobe nozzles had lowest internal losses at static conditions and 8-lobe nozzle with centerbody, shroud, and secondary air had least propulsive losses.
Transonic performance characteristics of several jet noise suppressors
NASA -- Tech Note
1960
48 pages
Report
English
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Transonic Drag of Several Jet-noise Suppressors
NTRS | 1958
|Transonic drag of several jet-noise suppressors
Engineering Index Backfile | 1958
|