SAE AIR5020 PDF

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Time-Dependent In-Flight Thrust Determination

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Description

The purpose and intent of Subcommittee E-33E’s effort, the reporting objectives, and the limitations inherent in the reported findings and recommendations are reviewed since these factors are the basis of the information contained in this document.
SAE E-33E Subcommittee was formed to assess the level of industry experience that exists in the area of thrust determination during aircraft time-variant operating conditions. A prime objective was to provide a center for gathering expertise and to be a forum for the exchange of ideas and viewpoints. The committee recognized that a practice for the rigorous treatment of time-dependent thrust did not exist and that several critical aspects of its accounting would need to be investigated.
The specific objectives of this document are:

a
To examine aircraft and engine operating conditions under which the quasi-steady thrust assumption is valid.

b
To determine the extent to which time-dependent (nonstationary) force accounting for engine net thrust and propulsion system throttle-dependent terms is required, consistent with existing and developing thrust-minus-drag techniques.

c
To report time-dependent thrust methodologies and measurement techniques used for flight and ground testing.

d
To present the results of a data review of state-of-the-art methodology appropriate to the determination of aircraft-installed thrust during quasi-steady and dynamic maneuvers.

e
To provide guidelines for validating and improving time-dependent thrust determination as appropriate to a specific program.

History

AIR5020A 2012-05-29 Latest Stabilized
AIR5020 2004-11-17 Historical Reaffirmed
ISSUING COMMITTEE

E-33 In Flight Propulsion Measurement Committee

DATE

2004-11-17

DOI

https://doi.org/10.4271/AIR5020

ISCURRENT
PAGE

161

PUBLISHER

SAE International

REVISED

REAFFIRMED

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SAE AIR5020 PDF
$186.00 Original price was: $186.00.$106.02Current price is: $106.02.