Experimental and Computational Investigation of a Dual-Bell Nozzle

Publication Year:
2014
Usage 3
Abstract Views 2
Downloads 1
Repository URL:
https://digitalcommons.wpi.edu/mqp-all/1124; https://digitalcommons.wpi.edu/cgi/viewcontent.cgi?article=2123&context=mqp-all
Author(s):
Fortner, Elizabeth Carr; McCallum, Hannah; Putzke, Hunter James; Davis, Katlin Bess; Heard, Michael Winlow
Publisher(s):
Worcester Polytechnic Institute
Tags:
Aerospace Engineering; Mechanical Engineering
artifact description
Increased interest in launching nanosatellites drives the development of alternative, more efficient, rocket nozzles. One such option is the dual-bell nozzle (DBN), in which the geometry is designed to achieve two ideal design points over the ascent profile, resulting in a higher average specific impulse for the booster stage. This project involved the design of a DBN, which was then modeled using ANSYS Fluent. A scaled DBN was also fabricated and tested in an indraft supersonic wind tunnel. Results from the experimental characterization of the DBN, using schlieren imaging of flow structures, are presented and found to be qualitatively consistent with simulation results. Results of the Fluent simulations for a full-scale DBN and the scaled DBN tested in the wind tunnel are also presented.