Dissertation/Thesis Abstract

Numerical Study and Investigation of a Gurney Flap Supersonic Nozzle
by El Mellouki, Mohammed, M.S., Mississippi State University, 2018, 100; 10979662
Abstract (Summary)

Flow separation is a common fluid dynamics phenomenon that occurs within supersonic nozzles while operating at off-design pressures. Typically, off-design pressures result in a shock formation that leads to a non-uniformity of the exiting flow and creates flow separation and flow recirculation. So far, no effective solution has been presented to eliminate flow separation and increase the total performance of the nozzle. The purpose of this work is to investigate whether a Gurney flap may beneficially affect the exiting flow pattern. For a better understanding of the Gurney flap effect, this investigation used a supersonic nozzle geometry based on a previous study by Lechevalier (2005). Results from the tested cases showed a poor effect of the flap at high free-stream Mach number and lower pressure ratio. Simulations of different flap heights along with different parameters showed a slight increase of thrust.

Indexing (document details)
Advisor: Janus, Mark J.
Commitee: Belk, Davy, Thompson, David S.
School: Mississippi State University
Department: Aerospace Engineering
School Location: United States -- Mississippi
Source: MAI 58/03M(E), Masters Abstracts International
Source Type: DISSERTATION
Subjects: Fluid mechanics, Engineering, Aerospace engineering
Keywords: Computational fluid dynamics, Flow separation, Fluid mechanics, Gurney flap, Supersonic nozzle
Publication Number: 10979662
ISBN: 9780438759220
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