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STEEL TUBING (WELDED) Chromium Molybdenum (.27 - .33 Carbon) (Normalized)
STEEL Nickel Molybdenum
STEEL Nickel Molybdenum
STEEL 1.8 Ni - .25 Mo (.38 - .43C) Heat Treated (105,000 TS)
STEEL COTTER PINS, GALVANIZED Low Carbon
Fault-Tree Generation for Embedded Software Implementing Dual-Path Checking
A New Policy for COTS Selection: Overcome the DSM Reliability Challenge
Visionary's Take: An Engineering Journey into the Marketplace (Part 3 of 3)
Visionary's Take: An Engineering Journey into the Marketplace (Part 1 of 3)
The Correlation of As-Manufactured Products to As-Designed Specifications: Closing the Loop on Dimensional Quality Results to Engineering Predictions
Secure Software Distribution in Aviation Context
Procedure for the Continuous Sampling and Measurement of Non-Volatile Particle Emissions from Aircraft Turbine Engines
Procedure for the Continuous Sampling and Measurement of Non-Volatile Particle Emissions from Aircraft Turbine Engines
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.