Correction: Three-Dimensional Spatio-Temporal Disturbance Flow Field Analysis of Particulate-Induced High-Speed Boundary-Layer Transition

S. M.A. Al Hasnine, V. Russo, A. Tumin, C. Brehm

Research output: Contribution to journalComment/debatepeer-review

Abstract

Correction Notice In Section VI.B., the acoustic modes are considered within the range of k=0.01-2.0. In Fig, 5, the color (red-blue) in the iso-volume pressure plot should be inverse. The correct figure is provided below (Image Presented).

Original languageEnglish (US)
Article numberAIAA 2021-1657.c1
JournalAIAA Scitech 2021 Forum
DOIs
StatePublished - 2021
EventAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021 - Virtual, Online
Duration: Jan 11 2021Jan 15 2021

ASJC Scopus subject areas

  • Aerospace Engineering

Fingerprint

Dive into the research topics of 'Correction: Three-Dimensional Spatio-Temporal Disturbance Flow Field Analysis of Particulate-Induced High-Speed Boundary-Layer Transition'. Together they form a unique fingerprint.

Cite this