TY - GEN
T1 - Characterization of Novel Large Amplitude Gust Generator
AU - Bricker, Clemence C.
AU - Bull, Sam
AU - Gursul, Ismet
AU - Young, Anna M.
PY - 2025/1/3
Y1 - 2025/1/3
N2 - Understanding the unsteady load response of a wing to a gust is of critical importance in aerodynamics. Many different designs of gust generator have therefore been built and tested in both wind and water tunnels, each design coming with distinct advantages and drawbacks. This study presents a cascade of 58 oscillating airfoils as a novel large amplitude gust generator. The gust produced was tested at different Reynolds numbers and reduced frequencies. It was found to be two-dimensional, uniform, and repeatable, and therefore representative of a Sears-type gust. In contrast to vortical gust generators such as plunging wing wakes, the new gust generator produces highly correlated gusts, even at low reduced frequencies. Large-amplitude, coherent, transverse velocity is superimposed by small-scale vorticity fluctuations in the wakes of the oscillating multi-vane cascade. Two airfoil sections, NACA 0012 and NACA 63-421, were then tested. The normalized lift amplitude was found to follow the theoretical Sears prediction.
AB - Understanding the unsteady load response of a wing to a gust is of critical importance in aerodynamics. Many different designs of gust generator have therefore been built and tested in both wind and water tunnels, each design coming with distinct advantages and drawbacks. This study presents a cascade of 58 oscillating airfoils as a novel large amplitude gust generator. The gust produced was tested at different Reynolds numbers and reduced frequencies. It was found to be two-dimensional, uniform, and repeatable, and therefore representative of a Sears-type gust. In contrast to vortical gust generators such as plunging wing wakes, the new gust generator produces highly correlated gusts, even at low reduced frequencies. Large-amplitude, coherent, transverse velocity is superimposed by small-scale vorticity fluctuations in the wakes of the oscillating multi-vane cascade. Two airfoil sections, NACA 0012 and NACA 63-421, were then tested. The normalized lift amplitude was found to follow the theoretical Sears prediction.
UR - http://www.scopus.com/inward/record.url?scp=105001409476&partnerID=8YFLogxK
U2 - 10.2514/6.2025-2765
DO - 10.2514/6.2025-2765
M3 - Chapter in a published conference proceeding
AN - SCOPUS:105001409476
SN - 9781624107238
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
BT - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
PB - American Institute of Aeronautics and Astronautics Inc.
CY - Virginia, U. S. A.
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
Y2 - 6 January 2025 through 10 January 2025
ER -