Adaptive Surrogate-Based Optimization of Vortex Generators for Tiltrotor Geometry
Author:
Affiliation:
1. University of Bristol, Bristol, England BS8 1TR, United Kingdom
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.C033838
Reference57 articles.
1. MaiselM.GiulianettiD.DuganD. “The History of the XV-15 Tilt Rotor Research Aircraft: From Concept to Flight,” NASA SP 2000-4517, 2000.
2. Review of research on low-profile vortex generators to control boundary-layer separation
3. WeibergM.MaiselJ. A. “Wind-Tunnel Tests of the XV-15 Tilt Rotor Aircraft,” NASA TM 81177, 1980.
4. Effect of Midwing Vortex Generators on V-22 Aircraft Forward-Flight Aerodynamics
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