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This content will become publicly available on January 3, 2026

Title: Online Feedback Flow Control for Finite Wings
Award ID(s):
2052811 2129494
PAR ID:
10629465
Author(s) / Creator(s):
; ; ;
Publisher / Repository:
American Institute of Aeronautics and Astronautics
Date Published:
ISBN:
978-1-62410-723-8
Format(s):
Medium: X
Location:
Orlando, FL
Sponsoring Org:
National Science Foundation
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