Details:

Creators:
Olmstead, Jeffrey R. ; Fleming, Gregg G. ; Gulding, John M. ; Roof, Christopher J. ; Gerbi, Paul J. ; ... More +
Olmstead, Jeffrey R. ; Fleming, Gregg G. ; Gulding, John M. ; Roof, Christopher J. ; Gerbi, Paul J. ; Rapoza, Amanda S. ; Less -
Corporate Creators:
John A. Volpe National Transportation Systems Center (U.S.). Acoustics Facility ; United States. Federal Aviation Administration. Office of Environment and Energy ;
John A. Volpe National Transportation Systems Center (U.S.). Acoustics Facility ; United States. Federal Aviation Administration. Office of Environment and Energy ; Less -
Subject/TRT Terms:
[+]
Computer Model
Day-night Average Sound Level
FAR Part 150
Heliport Noise Model
Integrated Noise Model
Ldn
Noise-level Metric
Noise-level Prediction
Noise Contours
Airport Noise
Computer Models
Heliports
Manuals
Measurement
Noise
Sound Level

Publication/ Report Number:
FAA-AEE-02-01 ;
Resource Type:
Manual ;
Geographical Coverage:
United States ;
Corporate Publisher:
John A. Volpe National Transportation Systems Center (U.S.) ;
NTL Classification:
NTL-AVIATION-Aviation Energy and Environment ; AGR-IMPACTS-Environment ; NTL-ENERGY AND ENVIRONMENT-Environment Impacts ; NTL-ENERGY AND ENVIRONMENT-Aviation Energy and Environment ;
Abstract:
The Federal Aviation Administration, Office of Environment and Energy (FAA, AEE-100) has developed Version 6.0 of the Integrated Noise Model (INM) with support from the John A. Volpe National Transportation Systems Center, Acoustics Facility (Volpe Center) for development of the acoustic computation module, and from the ATAC Corporation for systems integration, development of the graphical interface, and methods for computing aircraft flight profiles and constructing flight paths, which are processed by the acoustics module. This Technical Manual describes the core technical components in INM 6.0, including the flightpath methodology (Chapter 2), along with the basic methodology employed by the INM to compute noise levels or time-above metrics at a single, user-specified observer, or at an evenly-spaced, regular grid of observers (Chapter 3). The noise/time computation methodology includes a description of: (1) computation of the flightsegment geometric and physical parameters; (2) flight-segment noise-level interpolation process; (3) atmospheric absorption adjustment; (4) acoustic impedance adjustment; (5) flight-segment noise-fraction adjustment for exposure-based metrics; (6) aircraft speed adjustment for exposure-based metrics; (7) lateral attenuation adjustment; (8) ground-based directivity adjustment for observers behind start-of-takeoff-roll, as well as for computing metrics associated with run-up operations; (9) metric computation process; and (10) development of a recursively-subdivided irregular grid methodology, which is used for computing noise contours (Chapter 4).
Format:
PDF ;
Funding:
DTFA01-99-C-00003 ; FA265/A2012 ;
DTFA01-99-C-00003 ; FA265/A2012 ; Less -
Collection(s):
Volpe
Main Document Checksum:
[+]
urn:sha256:db9b8e74be5a2ab483d03ec029c576eef0e03d3be92ad1758b73e2a34b4663b3
File Type:

Supporting Files

• No Additional Files

More +