TY - GEN
T1 - ONTO QUANTIFYING UNSTEADY PROPULSION CHARECTERISTICS USING MOMENTUM AND ENERGY CONTROL VOLUME ASSESMENTS
AU - Loubimov, George
AU - Kinzel, Michael
N1 - Publisher Copyright:
© 2022 American Society of Mechanical Engineers (ASME). All rights reserved.
PY - 2022
Y1 - 2022
N2 - This work proposes a novel approach to characterize unsteady, undulating propulsion components through evaluating the momentum and energy equations using detailed control volume analyses. Specifically, it is difficult in such conditions to separate thrust from drag as pressure components are inseparable. In general, the goal is to link physical processes to various components in the control volume assessments that are measurable in detailed computational fluid dynamics (CFD) models. The effort utilizes the Method of Manufactured Solutions (MMS) to verify detailed insight can be extracted from the control volume assessments are developed and indicate that the energy equation uniquely highlights lift-work in the energy budget and separating propulsive and drag forces. The effort expands the findings to previously validated CFD studies studying thrust from heaving and pitching foils; results indicate a novel approach to separate the axial force into thrust and drag components. Overall, the results indicate a promising method useful to separate losses from propulsive mechanisms along with novel metrics of efficiencies useful to measuring self-propelling vehicles.
AB - This work proposes a novel approach to characterize unsteady, undulating propulsion components through evaluating the momentum and energy equations using detailed control volume analyses. Specifically, it is difficult in such conditions to separate thrust from drag as pressure components are inseparable. In general, the goal is to link physical processes to various components in the control volume assessments that are measurable in detailed computational fluid dynamics (CFD) models. The effort utilizes the Method of Manufactured Solutions (MMS) to verify detailed insight can be extracted from the control volume assessments are developed and indicate that the energy equation uniquely highlights lift-work in the energy budget and separating propulsive and drag forces. The effort expands the findings to previously validated CFD studies studying thrust from heaving and pitching foils; results indicate a novel approach to separate the axial force into thrust and drag components. Overall, the results indicate a promising method useful to separate losses from propulsive mechanisms along with novel metrics of efficiencies useful to measuring self-propelling vehicles.
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U2 - 10.1115/FEDSM2022-87219
DO - 10.1115/FEDSM2022-87219
M3 - Conference contribution
AN - SCOPUS:85139759623
T3 - American Society of Mechanical Engineers, Fluids Engineering Division (Publication) FEDSM
BT - Fluid Applications and Systems (FASTC); Fluid Measurement and Instrumentation (FMITC); Fluid Mechanics (FMTC)
PB - American Society of Mechanical Engineers (ASME)
T2 - ASME 2022 Fluids Engineering Division Summer Meeting, FEDSM 2022
Y2 - 3 August 2022 through 5 August 2022
ER -