TY - GEN
T1 - A computational study on avian flapping flight and the influence of feather separation
AU - Feaster, Jeffrey
AU - Battaglia, Francine
AU - Bayandor, Javid
PY - 2016
Y1 - 2016
N2 - Bird flight is an area of significant interest due to the utilization and control of unsteady aerodynamic effects via flapping Although modern aerodynamics were originally inspired by bird flight, contemporary computational and experimental work associated with flapping flight focuses on insect flight. The purpose of the present paper is to improve the understanding of avian flight by investigating upstroke downstroke velocities, feather separation, and ultimately develop a nondimensional model to predict lift and drag forces for seagull flight. The variation in upstroke-downstroke velocities were found to decrease both lift and drag as the relative upstroke velocity increased, but significantly increased the lift: drag ratio for the same flight regime. Feather separation was found to increase lift with maximum lift at a separation angle of 25°, while drag increased linearly. A set of nondimensional equations found were using regression analysis that can be used as a design tool to predict both lift and drag without expensive experiments or excessive computational processing requirements.
AB - Bird flight is an area of significant interest due to the utilization and control of unsteady aerodynamic effects via flapping Although modern aerodynamics were originally inspired by bird flight, contemporary computational and experimental work associated with flapping flight focuses on insect flight. The purpose of the present paper is to improve the understanding of avian flight by investigating upstroke downstroke velocities, feather separation, and ultimately develop a nondimensional model to predict lift and drag forces for seagull flight. The variation in upstroke-downstroke velocities were found to decrease both lift and drag as the relative upstroke velocity increased, but significantly increased the lift: drag ratio for the same flight regime. Feather separation was found to increase lift with maximum lift at a separation angle of 25°, while drag increased linearly. A set of nondimensional equations found were using regression analysis that can be used as a design tool to predict both lift and drag without expensive experiments or excessive computational processing requirements.
UR - https://www.scopus.com/pages/publications/85013652394
M3 - Conference contribution
AN - SCOPUS:85013652394
T3 - 30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016
BT - 30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016
PB - International Council of the Aeronautical Sciences
T2 - 30th Congress of the International Council of the Aeronautical Sciences, ICAS 2016
Y2 - 25 September 2016 through 30 September 2016
ER -