Unsteady aerodynamics of reverse flow dynamic stall on an oscillating blade section

Author:

Lind Andrew H.1ORCID,Jones Anya R.1ORCID

Affiliation:

1. Department of Aerospace Engineering, University of Maryland, College Park, Maryland 20740, USA

Funder

Penn State Vertical Lift Research Center of Excellence (PSU VLRCOE)

Publisher

AIP Publishing

Subject

Condensed Matter Physics,Fluid Flow and Transfer Processes,Mechanics of Materials,Computational Mechanics,Mechanical Engineering

Reference22 articles.

1. A. Bagai, “Aerodynamic design of the X2 technology demonstrator™ main rotor blade,” in64th Annual Forum of the AHS, 2008.

2. M. Mayo, V. Raghav, M. Barbley, B. Liberi, and N. Komerath, “Flow structure on a retreating rotor blade at high advance ratios,” in ASME 2014 International Mechanical Engineering Congress and Exposition, 2014.

3. Experimental Investigation and Fundamental Understanding of a Full-Scale Slowed Rotor at High Advance Ratios

4. Computational Investigation and Fundamental Understanding of a Slowed UH-60A Rotor at High Advance Ratios

5. M. Potsdam, H. Yeo, and R. A. Ormiston, “Performance and loads predictions of a slowed uh-60a rotor at high advance ratios,” in 39th European Rotorcraft Forum, 2013.

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