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Certification of Engine Health Management Systems: Guidelines for Selecting Software Assurance Levels
OBD Approval Process
Developing a System based on a COTS ARINC 653 Operating System
Spotlight on Design Insight: Fuel Efficiency: Fuel Economy Testing
How to Address the Existing and Future Requirements of ASFC: The Safe and Secure Virtualization RTOS Approach
Development and Demonstration of a Low Emissions Four-Stroke Outboard Marine Engine Utilizing Catalyst Technology
Wiley Cyber Security Collection Add-On
Advances in Catalyst Substrates, 2017
Advances in Catalyst Substrates, 2018
Special Considerations for the Application of IVHM to Autonomous Aircraft and Vehicles
Procedure for the Continuous Sampling and Measurement of Non-Volatile Particle Emissions from Aircraft Turbine Engines
This Aerospace Information Report (AIR) is a historical technical record describing procedures, required continuous sampling conditions, and instrumentation for the measurement of non-volatile particle number and mass concentrations from the exhaust of aircraft gas turbine engines. Procedures are included to calculate sampling loss performance. This AIR is not intended for in-flight testing, nor does it apply to engine operating in the afterburning mode.
This Aerospace Information Report is a historical technical record of the initial document detailing the measurement of non-volatile particle emissions at the exit plane of aircraft gas turbine engines. This methodology was adopted by ICAO into Annex 16 Vol II and updated into Aerospace Recommended Practice ARP6320.
Future updates of this document may include explanations of the reasoning and assumptions used to develop this measurement methodology.