Experimentally modified unsteady shock wave model for wave rotor design

  • Shining Chan*
  • , Huoxing Liu
  • *Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

Unsteady shock waves are vital to the compression in a wave rotor, and it is a main part of wave rotor design to predict the unsteady shock waves. The classical analytic model is capable of such prediction for ideal inviscid flow, but additional losses in the real viscous flow cause the properties of shock waves to diverge from that prediction. The analytic model was modified to correct such divergence via correlation coefficients, and was calibrated via experiment. The experiments were conducted in a single-channel experimental rig where unsteady shock waves could be tested with uniform incoming flow. Three similarity principles were investigated in the experiment. They determined the correlation coefficients in the modified model. The modified model would be applied to wave rotor design provided that the similarity principles of the wave rotor channel match those in the experiments.

Original languageEnglish
Title of host publication50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Electronic)9781624103032
DOIs
StatePublished - 2014
Event50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014 - Cleveland, United States
Duration: 28 Jul 201430 Jul 2014

Publication series

Name50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference 2014

Conference

Conference50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and exhibit 2014
Country/TerritoryUnited States
CityCleveland
Period28/07/1430/07/14

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