Two-Dimensional Numerical Study of Micronozzle Geometry

Two-Dimensional Numerical Study of Micronozzle Geometry

Supersonic micronozzles operate in the unique viscosupersonic flow regime, characterized by large Mach numbers (M>1) and low Reynolds numbers (Re<1000). Past research has primarily focused on the design and analysis of converging-diverging de Laval nozzles; however, plug (i.e. centerbody) desi...

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Bibliographic Details
Main Author: Pearl, Jason M.
Format: Others
Language:en
Published: ScholarWorks @ UVM 2016
Subjects:
Aerospike
Computational Fluid Dynamics
Micropropulsion
Plug Nozzle
Aerospace Engineering
Mechanical Engineering
Online Access:http://scholarworks.uvm.edu/graddis/579
http://scholarworks.uvm.edu/cgi/viewcontent.cgi?article=1578&amp;context=graddis

Internet

http://scholarworks.uvm.edu/graddis/579
http://scholarworks.uvm.edu/cgi/viewcontent.cgi?article=1578&amp;context=graddis

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