Performance tests and characteristics of short length, double annular ram induction turbojet combustion chambers for supersonic flight
Full scale tests of a short length, double annular ram induction turbojet combustor for supersonic flight
1971-03-01
Sonstige
Keine Angabe
Englisch
Effect of combustor-inlet conditions on performance of Annular Turbojet Combustor
Engineering Index Backfile | 1947
|Effect of combustor-inlet conditions on performance of annular turbojet combustor
Engineering Index Backfile | 1947
|