Performance of a vortex-controlled diffuser in an annular swirl-can combustor at inlet mach numbers up to 0.53
NASA technical paper ; 1452
1979
14 S.
Ill., graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Inlet swirl effects on dump combustor flows
AIAA | 1990
|Measurements in an annular combustor-diffuser system
AIAA | 1990
|