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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)
Vertical Picture-Frame Wing Jig Structure Design with an Eye to Foundation Loading
Vehicle Aerodynamics, 2015
Manufacturing/Materials/Structures, AeroTech 2015
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
Training Program Guidelines for Deicing/Anti-Icing of Aircraft on Ground
Effects of Reflux Temperature and Molarity of Acidic Solution on Chemical Functionalization of Helical Carbon Nanotubes
Stall Mitigation and Lift Enhancement of NACA 0012 with Triangle-Shaped Surface Protrusion at a Reynolds Number of 105
Conceptual Design, Material, and Structural Optimization of a Naval Fighter Nose Landing Gear for the Estimated Static Loads
ERRATA
Parametric Studies on Airfoil-Boundary Layer Ingestion Propulsion System
Flight Performance Envelope for an Aircraft with a Fixed-Pitch Propeller
Carbon Fiber/Epoxy Mold with Embedded Carbon Fiber Resistor Heater - Case Study
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.