Effect of off-body laser discharge on drag reduction of hemisphere cylinder in supersonic flow-part II

  • Nadia Kianvashrad
  • , Doyle Knight
  • , Stephen P. Wilkinson
  • , Amanda Chou
  • , George B. Beeler
  • , Moazzam Jangda

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

The interaction of on-axis and off-axis laser discharge in front of a hemisphere cylinder in Mach 2.0 flow is investigated numerically. Details of the physics of the interaction of the laser-induced shock and the heated region with the bow shock and its effect on drag reduction are included. The energetic efficiency of the laser discharge in reducing drag is calculated.

Original languageEnglish (US)
Title of host publicationAIAA Aerospace Sciences Meeting
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105241
DOIs
StatePublished - 2018
EventAIAA Aerospace Sciences Meeting, 2018 - Kissimmee, United States
Duration: Jan 8 2018Jan 12 2018

Publication series

NameAIAA Aerospace Sciences Meeting, 2018

Other

OtherAIAA Aerospace Sciences Meeting, 2018
Country/TerritoryUnited States
CityKissimmee
Period1/8/181/12/18

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

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