Performance at Simulated High Altitudes of a Prevaporizing Annular Turbojet Combustor Having Low Pressure Loss
1956
43 pages
Report
No indication
English
Combustor , Fuel combustion , Turbojet engine , Annulus , Atomization , Characteristics , Combustion , Engine , Fuel , High altitude , Jet , Low pressure , Performance , System , Turbojet , Vaporization
Effect of combustor-inlet conditions on performance of Annular Turbojet Combustor
Engineering Index Backfile | 1947
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