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ASME PTC55 : 2013

M00008372

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ASME PTC55 : 2013

GAS TURBINE AIRCRAFT ENGINES

American Society of Mechanical Engineers

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Table of Contents

Notice
Foreword
Committee Roster
Correspondence With the PTC Committee
Introduction
Section 1 - Object and Scope
Section 2 - Definitions and Descriptions
            of Terms
Section 3 - Guiding Principles
Section 4 - Instruments and Methods of
            Measurement
Section 5 - Computation of Results
Section 6 - Test Report Requirements
Section 7 - Uncertainty
Mandatory Appendix
I - Orifice Meters Installed in Pipes 2 in. (51 mm)
    Inside Diameter (I.D.) or Less
Nonmandatory Appendices
A - Conversion Factors
B - Sample Core Flow Calculations
C - Sample Liquid Fuel Calculations
D - Energy Transfer
E - Uncertainty Analysis Calculations
F - Measurement of Emission
G - Transient Testing
H - Bibliography

Abstract

Defines the performance testing of gas turbine aircraft engines at steady-state conditions. This Code applies to turbojet, turbofan, turboshaft, and turboprop engines.

General Product Information

Document Type Standard
Status Current
Publisher American Society of Mechanical Engineers