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The National Aeronautics and Space Administration (NASA), Langley
Research Center (LaRC) and the Environmental Measurement and
Modeling Division of the United States Department of
Transportation's John A. Volpe National Transportation Systems
Center (Volpe) conducted a noise measurement study to examine the
sound level directivity pattern behind aircraft start-of-takeoff
roll. This report discusses the procedures and methodologies used
to measure and quantify data acquired from the Study.
Sounds associated with oversnow vehicles, such as snowmobiles and
snowcoaches, are an important management concern at Yellowstone and
Grand Teton National Parks. The John A. Volpe National
Transportation Systems Center's Environmental Measurement and
Modeling Division is supporting the National Park Service with its
on-going Winter Use Planning program. As part of this support,
acoustic measurements of ten snowcoaches and six snowmobiles were
made at the south entrance to Yellowstone National Park from the
26th through the 28th of February 2008. Measurement methodologies
were guided by SAE J1161 and SAE J192. There were two primary
objectives: 1) to determine which snowcoaches had the Best
Available Technology (BAT) with respect to noise emissions, and 2)
to determine if there was a significant difference between
snowmobile sound levels when tested using two revisions of SAE
J192.
This study provides new insights into aircraft plume behavior that
greatly surpasses historic understanding, and data for more
accurate modeling of plume rise and spread from commercial aircraft
at airports. This final report completes individual analysis of the
LAX data set, initially reported in the related Preliminary Report
published in September 2002. Additional studies are planned (based
on available funding) to analyze potential changes in the derived
parameters due to site characteristics (e.g., elevation, weather
conditions) and will be reported on as the work continues.
Two procedures for adjusting as-measured test-day spectra to
reference day conditions - the Society of Automotive Engineers'
(SAE) Aerospace Recommended Practice (ARP) No. 866A (866A) and a
procedure utilizing pure-tone absorption equations, developed in
support of the International Organization for Standardization's
(ISO) 9613-1 and the American National Standards Institute's (ANSI)
S1.26-1995, and refined for application to one-third octave-band
data- were evaluated and compared. The ISO and ANSI pure-tone
absorption equations are identical to each other. The 866A
procedure historically has been used for atmospheric absorption
corrections for Federal Aviation Regulations (FAR) Part 36, Noise
Standards: Aircraft Type and Airworthiness Certification and
similar regulations of the International Civil Aviation
Organization (ICAO). The ISO/ANSI procedure analyzed herein is
under consideration for inclusion into harmonized regulations. This
document presents a comparison of data corrected to several
distances using the two different methodologies.
In March 1998, the Federal Highway Administration (FHWA) Office of
Natural Environment, released the FHWA Traffic Noise Model (FHWA
TNM) Version 1.0, a state-of-the-art computer program for highway
traffic noise prediction and analysis. Since then, the FHWA, with
assistance from the Volpe Center Acoustics Facility (Volpe Center)
and Foliage Software Systems (FSS), have released updates of TNM
(Versions 1.0a, and 1.0b) in March 1999 and August 1999,
respectively. In support of the FHWA and the California Department
of Transportation, the Volpe Center and FSS released Version 1.1 in
September 2000. TNM 2.0 is the latest release of the TNM software.
Two companion reports were released with TNM Version 1.0, a
Technical Manual that describes the acoustics within TNM and a
User's Guide. In addition, prior to TNM release, a data report was
published that describes the vehicle noise-emissions data base
within TNM. This document is an addendum to the FHWA TNM Version
1.0 User's Guide. It details the enhancements in the program up to
and including Version 2.0.
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