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Applicability of Fly Neighborly Noise Recommendations to UAM Quadrotors Undergoing Steady ManeuversThis initial study examines whether the Helicopter Association International (HAI) Fly Neighborly operational recommendations that are based on single main rotor/tail rotor configurations will hold for non-conventional UAM rotorcraft with multiple rotors. The 6-occupant quadrotor concept vehicle designed under the NASA Revolutionary Vertical Lift Technology (RVLT) Project is studied. The tip speed is 550 ft/sec, with three blades per rotor (“550/3”). Predictions are made for three steady maneuvers: level turns, descending turns, and climbing turns. The RVLT Toolchain is exercised using CAMRAD II, pyaaron/AARON/ANOPP2 and a beta version of AMAT (ANOPP2 Mission Analysis Tool). AMAT provides functionality to acoustically model the curved flight paths associated with maneuvers. In addition to quadrotor trim and performance, this study includes analysis of azimuthal variations of the vertical blade loading and its derivative in the form of contour plots on a rotor plane and line plots at one radial location (r/R=0.765). Quadrotor noise trends are analyzed using maximum Overall Sound Pressure Level (OASPL) and Effective Perceived Noise Level (EPNL). The Fly Neighborly guideline that addresses descents (“Level turns are quieter than descending turns”) is predicted to hold for the RVLT Quadrotor as well.
Document ID
20240000099
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Sesi Kottapalli
(Ames Research Center Mountain View, United States)
Christopher Silva
(Ames Research Center Mountain View, United States)
D Douglas Boyd Jr.
(Langley Research Center Hampton, United States)
Date Acquired
January 3, 2024
Subject Category
Aeronautics (General)
Meeting Information
Meeting: Transformative Vertical Flight 2024, 11th Annual Electric VTOL Symposium, 6th Decennial VFS Aeromechanics Specialists' Conference
Location: Santa Clara, CA
Country: US
Start Date: February 6, 2024
End Date: February 8, 2024
Sponsors: VFS - The Vertical Flight Society
Funding Number(s)
WBS: 664817
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
UAM
Quadrotors
Helicopter
RVLT
Acoustics
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