Rotorcraft Performance Model (RPM) for use in AEDT.

Senzig, David A.; Boeker, Eric R.; John A. Volpe National Transportation Systems Center (U.S.)

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Rotorcraft Performance Model (RPM) for use in AEDT.

2015-11-01
By Senzig, David A. ; Boeker, Eric R.

[PDF-1.12 MB]

English

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Details:

Creators:

Senzig, David A. ; Boeker, Eric R.

Senzig, David A. ; Boeker, Eric R. Less -
Corporate Creators:

John A. Volpe National Transportation Systems Center (U.S.)
Corporate Contributors:

United States. Department of Transportation. Federal Aviation Administration. Office of Environment and Energy
Subject/TRT Terms:

[+]

Aircraft Exhaust Gases Aircraft Noise Aviation Environmental Design Tool Fuel Consumption Helicopter Performance Helicopters Noise Models Physics Rotary Wing Aircraft
Publication/ Report Number:

DOT-VNTSC-FAA-16-03
Resource Type:

Tech Report
Geographical Coverage:

United States
Corporate Publisher:

John A. Volpe National Transportation Systems Center (U.S.)
Abstract:

This report documents a rotorcraft performance model for use in the FAA’s Aviation Environmental Design Tool. The new rotorcraft performance model is physics-based. This new model replaces the existing helicopter trajectory modeling methods in the Aviation Environmental Design Tool which were mode-based. The new methods enable fuel consumption and emissions modeling based on the performance data derived from information found in the helicopters’ flight manuals.
Format:

PDF
Funding:

FA5JC6/PJ1C1
Collection(s):

Volpe Center
Main Document Checksum:

[+]

urn:sha256:e5a7ae6c41f6b5df63eed08c8dbaacb71d1a1493a42a4977017eba2fe63fe021
Download URL:

https://rosap.ntl.bts.gov/view/dot/12235/dot_12235_DS1.pdf
File Type:

No Additional Files

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Rotorcraft Performance Model (RPM) for use in AEDT.

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