COMPUTATIONAL COMBUSTION MODEL OF THRUST AUGMENTOR FOR AIRBREATHING ENGINES
23rd Aerospace Sciences Meeting ; 1985 ; Reno , NV , U.S.A.
1985-01-01
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Thrust augmentor inlet optimization
AIAA | 1986
|NTIS | 1971
|Spin Nozzle and Thrust Augmentor Mechanism
NTIS | 1975
|Reversed cowl flap inlet thrust augmentor
NTRS | 1975
|