ASME PTC55 : 2013
ASME PTC55 : 2013
GAS TURBINE AIRCRAFT ENGINES
American Society of Mechanical Engineers
GAS TURBINE AIRCRAFT ENGINES
American Society of Mechanical Engineers
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
Defines the performance testing of gas turbine aircraft engines at steady-state conditions. This Code applies to turbojet, turbofan, turboshaft, and turboprop engines.
Document Type | Standard |
Status | Current |
Publisher | American Society of Mechanical Engineers |