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