High lift INflight VAlidation (HINVA) - Overview about the 2nd Flight Test Campaign
Author:
Affiliation:
1. German Aerospace Center (DLR)
2. Airbus
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-0041
Reference17 articles.
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Aided Inertial Estimation of Wing Shape;Journal of Guidance, Control, and Dynamics;2021-02
2. An in-flight investigation of a turbulent boundary layer at Reynolds numbers up to $$\hbox {Re}_{\theta }=49,400$$;Experiments in Fluids;2020-12-23
3. Full-Scale In-Flight Flow Investigation of a High-Lift Vortex System by Means of Particle Image Velocimetry;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2017-10-31
4. An Autonomous, Traversable Boundary-Layer Probe for Flight Testing;54th AIAA Aerospace Sciences Meeting;2016-01-02
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