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Helicopter and Urban Air Mobility (UAM) Laboratory Comparison (HULC) Psychoacoustic Test The Helicopter and Urban Air Mobility (UAM) Laboratory Comparison (HULC) psychoacoustic test was conducted in July 2025 to compare human annoyance responses to noise from UAM vehicles and helicopters. This document provides a literature review, describes the HULC test methodology including stimuli selection and test administration procedures, and presents results from an initial analysis using multilevel statistical modeling. The test utilized 123 sound stimuli from four helicopters and six UAM vehicles across three flight phases (departure, cruise, and approach), presented to 40 subjects in the Exterior Effects Room (EER) at NASA's Langley Research Center. Subjects rated their annoyance on a 0 to 10 scale while imagining hearing these sounds multiple times daily near their homes. Key findings revealed that, at the same A-weighted sound exposure levels, UAM vehicles and helicopters produced similar annoyance responses across all flight phases, with mean differences of only approximately 1 dB and overlapping confidence intervals. However, at equivalent observer distances, UAM vehicles had inherently quieter operations and lower mean annoyance ratings. These results suggest that UAM vehicles and helicopters may be assessed in a similar manner for community noise impact. The quieter noise characteristics of UAM vehicles may provide advantages for operating in communities and integrating into urban environments.
Document ID
20250008984
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Aaron B Vaughn
(Langley Research Center Hampton, United States)
Siddhartha Krishnamurthy
(Langley Research Center Hampton, United States)
Aric R Aumann
(Analytical Services & Materials (United States) Hampton, United States)
Brian C Tuttle
(Analytical Mechanics Associates (United States) Hampton, United States)
Andrew W Christian
(Langley Research Center Hampton, United States)
Date Acquired
September 4, 2025
Publication Date
February 1, 2026
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Acoustics
Report/Patent Number
NASA/TM-20250008984
Funding Number(s)
WBS: 664817.02.07.03.02.03
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
psychoacoustics
rotorcraft
helicopter
Urban Air Mobility
UAM
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