Heat-Flux Gauge Studies of Compressible Dynamic Stall
Author:
Affiliation:
1. Naval Postgraduate School, Monterey, California 93943
2. NASA Ames Research Center, Moffett Field, California 94035-1000
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.2019
Reference12 articles.
1. Competing Mechanisms of Compressible Dynamic Stall
2. Investigation of incipient dynamic stall over pitching airfoils using hot-film sensors
3. Measurement of unsteady boundary layer developed on an oscillating airfoil using multiple hot-film sensors
4. Pitch Rate and Reynolds Number Effects on Unsteady Boundary-Layer Transition and Separation
5. Unsteady separation processes and leading edge vortex precursors - Pitch rate and Reynolds number influences
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1. Infrared thermography for boundary layer transition measurements;Measurement Science and Technology;2020-09-25
2. Time-Frequency Analysis and Transitional Boundary Layer Investigation over a Pitching Airfoil;Scientia Iranica;2020-05-19
3. Transitional boundary layer study over an airfoil in combined pitch-plunge motions;Aerospace Science and Technology;2020-03
4. Unsteady Boundary Layer Transition Detection by Automated Analysis of Hot Film Data;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2017-10-31
5. Differential infrared thermography for boundary layer transition detection on pitching rotor blade models;Experiments in Fluids;2015-01-31
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