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Start Over Graduate Program Aerospace Engineering Year 2009 Keyword Computational Fluid Dynamics

1. The Use of Adjoint Methods in Jet Nozzle Design

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Open Access

Author:: Sikarwar, Nidhi
Title:: The Use of Adjoint Methods in Jet Nozzle Design
Graduate Program:: Aerospace Engineering
Keywords:: Noise Reduction
Adjoint Method
Computational Fluid Dynamics
Nozzle Design
File:: Download Sikarwar_Nidhi_Masters_Thesis.pdf
Committee Members:: Philip John Morris, Thesis Advisor/Co-Advisor
Philip John Morris, Thesis Advisor/Co-Advisor