shock @ exit mach contour.jpg size: 0.103722 MB
nozzel.wbpj size: 0.321158 MB
shock @ exit pressure contour .jpg size: 0.088785 MB
shock @ exit pressure xy.jpg size: 0.097944 MB
shock @ exit mach xy.jpg size: 0.070571 MB
shock insise mach contour.jpg size: 0.201158 MB
shock insise pressure contour.jpg size: 0.107648 MB
shock insise mach xy.jpg size: 0.099675 MB
shock insise pressure xy.jpg size: 0.095046 MB
Shock.jpg size: 0.12486 MB
subsonic pressure contour.jpg size: 0.18863 MB
subsonic velocity contour.jpg size: 0.202071 MB
super sonic mach xy.jpg size: 0.070191 MB
super sonic mach contour.jpg size: 0.387423 MB
super sonic pressure xy.jpg size: 0.094348 MB
super sonic pressure contour.jpg size: 0.341454 MB
nozzel.wbpj size: 0.321158 MB
shock @ exit pressure contour .jpg size: 0.088785 MB
shock @ exit pressure xy.jpg size: 0.097944 MB
shock @ exit mach xy.jpg size: 0.070571 MB
shock insise mach contour.jpg size: 0.201158 MB
shock insise pressure contour.jpg size: 0.107648 MB
shock insise mach xy.jpg size: 0.099675 MB
shock insise pressure xy.jpg size: 0.095046 MB
Shock.jpg size: 0.12486 MB
subsonic pressure contour.jpg size: 0.18863 MB
subsonic velocity contour.jpg size: 0.202071 MB
super sonic mach xy.jpg size: 0.070191 MB
super sonic mach contour.jpg size: 0.387423 MB
super sonic pressure xy.jpg size: 0.094348 MB
super sonic pressure contour.jpg size: 0.341454 MB
Reading Mode
C-d nozzel CFD Simulation
NoAI: This model, simulation, images, or project may not be utilized within datasets, during the developmental process, or as inputs for generative AI programs.
this project describes the behavior of the flow of the air in a C-D Nozzle with the changes in the back pressure