Large Eddy Simulation of Hypersonic Cold Wall Flat Plate-Part II

Nadia Kianvashrad, Doyle Knight

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

Abstract

In this paper, we evaluate the newly introduced Ht &p method for the prediction of hypersonic flat plate boundary layers. The effects of Mach number and wall temperature are examined as part of the validation. The prediction of Law of Wall, Reynolds Analogy Factor, turbulent Prandtl number, Morkovin, Huang and extended Strong Reynolds Analogy, turbulent shear and normal stresses, power spectrum are in agreement with the theory and available experimental and DNS data. The compressibility effects proved to be significant for the cases examined in this paper.

Original languageEnglish (US)
Title of host publicationAIAA SciTech Forum 2022
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624106316
DOIs
StatePublished - 2022
EventAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 - San Diego, United States
Duration: Jan 3 2022Jan 7 2022

Publication series

NameAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022

Conference

ConferenceAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Country/TerritoryUnited States
CitySan Diego
Period1/3/221/7/22

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

Fingerprint

Dive into the research topics of 'Large Eddy Simulation of Hypersonic Cold Wall Flat Plate-Part II'. Together they form a unique fingerprint.

Cite this