Results 121 to 130 of about 8,406 (224)

Comparative analysis of compressible solver schemes for underexpanded jet aerodynamics with Schlieren validation. [PDF]

open access: yesSci Rep
Alsaedi SS   +6 more
europepmc   +1 more source

Using shock generator for the fuel mixing of the extruded single 4-lobe nozzle at supersonic combustion chamber. [PDF]

open access: yesSci Rep
Alizadeh A   +8 more
europepmc   +1 more source

Home - About - Disclaimer - Privacy