Reducing noise from supersonic jets using linear feedback control informed by resolvent analysis
type: CreativeWork
description: Submission published under a 24 month embargo labeled 'U of I Access', the embargo will last until 2027-05-01
abstract: Submission published under a 24 month embargo labeled 'U of I Access', the embargo will last until 2027-05-01
author: Murthy, Sandeep Ravikumar
language: en
language: eng
keywords: Jet Noise Reduction, Resolvent analysis, Linear feedback control, Shock-laden flow, Supersonic flow, Turbuelnt flow
date published: 2025-02-17
date modified: 2026-07-22T22:25:05Z
provider: University of Illinois - Urbana-Champaign
publisher: Networked Digital Library of Theses and Dissertations
type: WebPage
source organization: University of Illinois Urbana-Champaign

PropertyValue
property ID: Handle
value: https://hdl.handle.net/2142/129487