Gust Induced Aerodynamic Force Prediction on a Transport Wing Using Quasi-Steady Approximation

DOI10.1142/S0219876215500346zbMath1359.76170OpenAlexW2205410601MaRDI QIDQ2972045

J. Bruce Ralphin Rose, Gr Jinu

Publication date: 7 April 2017

Published in: International Journal of Computational Methods (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1142/s0219876215500346

zbMATH Keywords

turbulenceCFDgust responsewind tunnel testingV-n diagram

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25)

Cites Work

• Aeroelastic design optimization for laminar and turbulent flows
• A General Continuous Sensitivity Equation Formulation for thek-εModel of Turbulence
• Aeroelastic instability and response of advanced aircraft wings at subsonic flight speeds

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