6 datasets found

Publisher version : http://pof.aip.org/resource/1/phfle6/v21/i6/p064108_s1?isAuthorized=no

Publisher version : http://pof.aip.org/resource/1/phfle6/v22/i1/p014102_s1?isAuthorized=no

Publisher version : http://pof.aip.org/resource/1/phfle6/v22/i11/p114102_s1?isAuthorized=no

Secondary injection into the divergent section of a supersonic rocket nozzle is investigated for the fluidic thrust vectoring effects. The study was conducted in the...

10 pages

Boundary layer separation from flaps is responsible for large performance losses during take-off and landing phases of an aeroplane flight, including loss of lift and...