Compressible Boundary-Layer Stability Calculations for Sweptback Wings with Suction
type: Item
instance of: scholarly article
title: Compressible Boundary-Layer Stability Calculations for Sweptback Wings with Suction
zbMATH Open document ID: 0486.76091
DOI: 10.2514/3.51080
author: Leslie M. Mack
published in: AIAA Journal
publication date: 1982-01-01T00:00:00Z
Mathematics Subject Classification ID: 76N20
Mathematics Subject Classification ID: 76M99
Mathematics Subject Classification ID: 76E99
zbMATH DE Number: 3765437
zbMATH Keywords: wings of infinite span
zbMATH Keywords: compressible, parallel-flow stability theory
zbMATH Keywords: supercritical
zbMATH Keywords: sweep angle of 23 deg, 35 deg
zbMATH Keywords: maximum spatial amplification rate
zbMATH Keywords: suction
zbMATH Keywords: maximum amplification rate
MaRDI profile type: Publication
full work available at URL: https://doi.org/10.2514/3.51080
OpenAlex ID: W2074430108
description: scientific article