Aerodynamic performance of the NREL Unsteady Aerodynamics Experiment (Phase IV) twisted rotor

Tom L Acker, M. Maureen Hand

Research output: Chapter in Book/Report/Conference proceedingConference contribution

1 Citation (Scopus)

Abstract

A great deal of experimental data has been obtained from operation of the Unsteady Aerodynamics Experiment at the National Renewable Energy Laboratory (NREL) in Golden, Colorado. This paper presents the results of analyzing data taken during Phase IV (1997) of the experiment in order to determine the baseline aerodynamic performance of the Phase IV twisted rotor. Plots of normal force coefficient versus angle of attack show that the performance of the twisted rotor at low angle of attack is similar to that predicted by wind tunnel tests. However, as the angle of attack is increased beyond the static stall angle there is significant overshoot in the lift. Measurements of the flow angle by five-hole pressure probes demonstrated that the angle of attack remains relatively uniform along the span of the rotor, and that there is a significant spanwise component of the flow over the rotor. A preliminary investigation into the occurrence of dynamic stall on the rotor indicates that the frequency of dynamic stall events significantly less on the twisted rotor as compared to the Phase II untwisted blade.

Original languageEnglish (US)
Title of host publication37th Aerospace Sciences Meeting and Exhibit
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
StatePublished - 1999
Event37th Aerospace Sciences Meeting and Exhibit, 1999 - Reno, United States
Duration: Jan 11 1999Jan 14 1999

Other

Other37th Aerospace Sciences Meeting and Exhibit, 1999
CountryUnited States
CityReno
Period1/11/991/14/99

Fingerprint

unsteady aerodynamics
renewable energy
aerodynamics
rotors
Aerodynamics
Rotors
angle of attack
Angle of attack
wind tunnel
energy
experiment
Experiments
probe
wind tunnel tests
pressure sensors
blades
Turbomachine blades
Wind tunnels
laboratory
plots

ASJC Scopus subject areas

  • Space and Planetary Science
  • Aerospace Engineering

Cite this

Acker, T. L., & Hand, M. M. (1999). Aerodynamic performance of the NREL Unsteady Aerodynamics Experiment (Phase IV) twisted rotor. In 37th Aerospace Sciences Meeting and Exhibit American Institute of Aeronautics and Astronautics Inc, AIAA.

Aerodynamic performance of the NREL Unsteady Aerodynamics Experiment (Phase IV) twisted rotor. / Acker, Tom L; Hand, M. Maureen.

37th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA, 1999.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Acker, TL & Hand, MM 1999, Aerodynamic performance of the NREL Unsteady Aerodynamics Experiment (Phase IV) twisted rotor. in 37th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA, 37th Aerospace Sciences Meeting and Exhibit, 1999, Reno, United States, 1/11/99.
Acker TL, Hand MM. Aerodynamic performance of the NREL Unsteady Aerodynamics Experiment (Phase IV) twisted rotor. In 37th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA. 1999
Acker, Tom L ; Hand, M. Maureen. / Aerodynamic performance of the NREL Unsteady Aerodynamics Experiment (Phase IV) twisted rotor. 37th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics Inc, AIAA, 1999.
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