Correction: Stability analysis of the flow fields of forced and unforced cylinders in crossflow (American Institute of Aeronautics and Astronautics Inc, AIAA)

Doron Schwartz; Michael Karp

doi:10.2514/6.2025-1488.c1

Correction: Stability analysis of the flow fields of forced and unforced cylinders in crossflow (American Institute of Aeronautics and Astronautics Inc, AIAA)

Doron Schwartz, Michael Karp

Aerospace Engineering

Technion - Israel Institute of Technology

Research output: Contribution to journal › Comment/debate

Abstract

Correction Notice In figures 5, 6, 9, 10, 12 and 14, the reference length-scale δ₉₉ is the boundary layer thickness at an angle of 60° (i.e. δ₉₉|_θ=60°), not at an angle of 90°.

Original language	English
Journal	AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
DOIs	https://doi.org/10.2514/6.2025-1488.c1
State	Published - 2025
Event	AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025 - Orlando, United States Duration: 6 Jan 2025 → 10 Jan 2025

All Science Journal Classification (ASJC) codes

Aerospace Engineering

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10.2514/6.2025-1488.c1

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title = "Correction: Stability analysis of the flow fields of forced and unforced cylinders in crossflow (American Institute of Aeronautics and Astronautics Inc, AIAA)",

abstract = "Correction Notice In figures 5, 6, 9, 10, 12 and 14, the reference length-scale δ99 is the boundary layer thickness at an angle of 60° (i.e. δ99|θ=60°), not at an angle of 90°.",

author = "Doron Schwartz and Michael Karp",

note = "Publisher Copyright: {\textcopyright} 2025 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.; AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025 ; Conference date: 06-01-2025 Through 10-01-2025",

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TY - JOUR

T1 - Correction

T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025

AU - Schwartz, Doron

AU - Karp, Michael

PY - 2025

Y1 - 2025

N2 - Correction Notice In figures 5, 6, 9, 10, 12 and 14, the reference length-scale δ99 is the boundary layer thickness at an angle of 60° (i.e. δ99|θ=60°), not at an angle of 90°.

AB - Correction Notice In figures 5, 6, 9, 10, 12 and 14, the reference length-scale δ99 is the boundary layer thickness at an angle of 60° (i.e. δ99|θ=60°), not at an angle of 90°.

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U2 - 10.2514/6.2025-1488.c1

DO - 10.2514/6.2025-1488.c1

M3 - تعليقَ / نقاش

JO - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022

JF - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022

Y2 - 6 January 2025 through 10 January 2025

ER -

Correction: Stability analysis of the flow fields of forced and unforced cylinders in crossflow (American Institute of Aeronautics and Astronautics Inc, AIAA)

Abstract

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