Aeroelastic wing performance in high intensity turbulence: integral length scale effects
Aeroelastic wing performance in high intensity turbulence: integral length scale effects
The impact of variations in the integral length scale of incoming free-stream turbulence onan aeroelastic NACA0012 wing is investigated using force, moment and PIV measurements. Ata chord-based Reynolds number (
Free Stream Turbulence, Aircraft Wing Design, Aviation Risk, Aerodynamic Performance, Unmanned Aerial Vehicle, Flow Conditions, NACA 0012, Power Spectral Density, Proper Orthogonal Decomposition, Structural Displacement
1789-1799
Thompson, Craig
f6a694f9-2c34-4baf-bd66-d8152432c277
Biler, Hulya
70228dd8-d797-4d5d-82c0-48b5b67eb55a
Symon, Sean
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Ganapathisubramani, Bharathram
5e69099f-2f39-4fdd-8a85-3ac906827052
May 2025
Thompson, Craig
f6a694f9-2c34-4baf-bd66-d8152432c277
Biler, Hulya
70228dd8-d797-4d5d-82c0-48b5b67eb55a
Symon, Sean
2e1580c3-ba27-46e8-9736-531099f3d850
Ganapathisubramani, Bharathram
5e69099f-2f39-4fdd-8a85-3ac906827052
Thompson, Craig, Biler, Hulya, Symon, Sean and Ganapathisubramani, Bharathram
(2025)
Aeroelastic wing performance in high intensity turbulence: integral length scale effects.
AIAA Journal, 63 (5), .
(doi:10.2514/1.J064015).
Abstract
The impact of variations in the integral length scale of incoming free-stream turbulence onan aeroelastic NACA0012 wing is investigated using force, moment and PIV measurements. Ata chord-based Reynolds number (
Text
Thompson et al 2025
- Accepted Manuscript
More information
Accepted/In Press date: 6 November 2024
e-pub ahead of print date: 7 February 2025
Published date: May 2025
Keywords:
Free Stream Turbulence, Aircraft Wing Design, Aviation Risk, Aerodynamic Performance, Unmanned Aerial Vehicle, Flow Conditions, NACA 0012, Power Spectral Density, Proper Orthogonal Decomposition, Structural Displacement
Identifiers
Local EPrints ID: 498907
URI: http://eprints.soton.ac.uk/id/eprint/498907
ISSN: 0001-1452
PURE UUID: f6862454-d0dd-439d-b167-8647dc2fb70a
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Date deposited: 04 Mar 2025 18:05
Last modified: 18 Sep 2025 01:44
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Contributors
Author:
Craig Thompson
Author:
Hulya Biler
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