Compressible Boundary-Layer Stability Calculations for Sweptback Wings with Suction

DOI10.2514/3.51080zbMath0486.76091OpenAlexW2074430108MaRDI QIDQ3947367

Leslie M. Mack

Publication date: 1982

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.51080

zbMATH Keywords

suctionsupercriticalwings of infinite spancompressible, parallel-flow stability theorymaximum amplification ratemaximum spatial amplification ratesweep angle of 23 deg, 35 deg

Mathematics Subject Classification ID

Hydrodynamic stability (76E99) Basic methods in fluid mechanics (76M99) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (3)

Effects of suction and wall shaping on the fundamental parametric resonance in boundary layers ⋮ Compressible boundary-layer stability theory ⋮ Linear stability of three-dimensional boundary layers

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