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Evaluation of a Combined Momentum Theory and Simple Vortex Theory (CMTSVT) Inflow Model for UAM Applications

Hariani, Jahnvi and Güner, Feyyaz and Prasad, J.V.R. (2022) Evaluation of a Combined Momentum Theory and Simple Vortex Theory (CMTSVT) Inflow Model for UAM Applications. VFS Aeromechanics for Advanced Vertical Flight Technical Meeting, 2022-01-25 - 2022-01-27, San Jose, CA, USA.

Full text not available from this repository.

Abstract

This paper uses the combined momentum and simple vortex theory (CMTSVT) inflow model to study effects of rotor-on-rotor interference on induced power predictions for different multirotor configurations. It builds upon the previously completed validation with the Harrington coaxial rotor which showed that this simple analytical model could capture the overall rotor-on-rotor wake interference effects in the rapid estimation of rotor power without coupling it with a blade element rotor model. Since it has already been shown that the CMTSVT inflow model can serve as a viable tool in the early design stages of vehicle configuration and sizing trade studies, this paper focuses on applying this model to analyze the effect of rotor arrangement on individual rotor performance, using the plus and cross quad-rotor configurations. Power predictions based on self-induced and interference inflow are included, in addition to first harmonic inflow components to gain further insight. A comparison of the obtained results with existing literature on rotor arrangement sensitivity further validates the applicability of the CMTSVT inflow model in rapid estimation of rotor-on-rotor inflow interference and its effect on rotor power for its use in the early design phases of advanced multi-rotor vehicle configurations.

Item URL in elib:https://elib.dlr.de/194068/
Document Type:Conference or Workshop Item (Speech)
Title:Evaluation of a Combined Momentum Theory and Simple Vortex Theory (CMTSVT) Inflow Model for UAM Applications
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Hariani, JahnviGeorgia Institute of TechnologUNSPECIFIEDUNSPECIFIED
Güner, FeyyazUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Prasad, J.V.R.School of Aerospace Engineering, Atlanta, usUNSPECIFIEDUNSPECIFIED
Date:27 January 2022
Refereed publication:No
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:pp. 1-10
Status:Published
Keywords:helicopter, aerodynamic interaction, induced inflow, multi-rotor inflow model, combined momentum theory and simple vortex theory
Event Title:VFS Aeromechanics for Advanced Vertical Flight Technical Meeting
Event Location:San Jose, CA, USA
Event Type:international Conference
Event Start Date:25 January 2022
Event End Date:27 January 2022
Organizer:Vertical Flight Society
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Efficient Vehicle
DLR - Research area:Aeronautics
DLR - Program:L EV - Efficient Vehicle
DLR - Research theme (Project):L - Virtual Rotorcraft and Validation
Location: Braunschweig
Institutes and Institutions:Institute of Flight Systems > Rotorcraft
Institute of Flight Systems
Deposited By: van der Wall, Prof. Dr. Berend G.
Deposited On:25 Apr 2023 12:51
Last Modified:24 Apr 2024 20:54

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