Correction to: Optimization of an Axisymmetric Mach 6 Reflected-Shock Tunnel Nozzle at Flight Enthalpy (AIAA Scitech 2021 Forum)

Ahsan Hameed, Muhammad Mustafa, David Shekhtman, Nick Parziale

Research output: Contribution to journalComment/debate

Abstract

Correction Notice Revised reference list (see pages below) that uses bracketed numbers in place of footnotes so that Google Scholar properly identifies and lists the references.

Original languageEnglish
Article numberAIAA 2021-0386.c1
JournalAIAA Scitech 2021 Forum
DOIs
StatePublished - 2021
EventAIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2021 - Virtual, Online
Duration: 11 Jan 202115 Jan 2021

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