High-speed PIV applied to wake of NASA CRM model at high Re-number sub- and transonic stall conditions

Within the framework of the EU project ESWIRP, the particle image velocimetry (PIV) using high-speed camera and laser has been used to measure the turbulent flow in the wake of a stalled aircraft wing. The measurements took place on the common research model provided by NASA in the pressurized cryog...

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Veröffentlicht in:	CEAS aeronautical journal 2018-06, Vol.9 (2), p.339-346
Hauptverfasser:	Konrath, Robert, Geisler, Reinhard, Agocs, Janos, Ehlers, Hauke, Philipp, Florian, Quest, Jürgen
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aerospace Technology and Astronautics Computational fluid dynamics Engineering High speed cameras Original Paper Particle image velocimetry Stalling Subsonic aircraft Turbulent flow Velocity measurement Wind tunnels Wings (aircraft)
Online-Zugang:	Volltext
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