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NICKEL ALLOY, CORROSION AND HEAT RESISTANT, SHEET, STRIP, AND PLATE 72Ni - 15.5Cr - 0.95(Cb + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted Solution Heat Treated, Precipitation Hardenable
ALLOY SHEET, STRIP, AND PLATE, CORROSION AND HEAT RESISTANT 72Ni - 15.5Cr - 0.95(Cb + Ta) - 2.5Ti - 0.70Al - 7.0Fe Consumable Electrode or Vacuum Induction Melted Solution Heat Treated, Precipitation Hardenable
Developing a System based on a COTS ARINC 653 Operating System
Spotlight on Design Insight: Fuel Efficiency: Fuel Economy Testing
Wiley Cyber Security Collection Add-On
COTTER PINS, METRIC Corrosion and Heat Resistant Steel 18Cr - 10.5Ni - 0.40Ti
COTTER PINS, METRIC, STEEL, CORROSION AND HEAT RESISTANT 18Cr - 10.5Ni - 0.40Ti
COTTER PINS, METRIC, CORROSION AND HEAT RESISTANT STEEL 18Cr - 10.5Ni - 0.40Ti
COTTER PINS, METRIC, STEEL, CORROSION AND HEAT RESISTANT 18Cr - 10.5Ni - 0.40Ti
Using Numerical Simulation to Obtain Length of Constant Area Section in Scramjet Combustor
Analytical Estimation of Infrared Signature of Converging and Converging-Diverging Nozzles of Jet Engine
Steel, Corrosion-Resistant, Bars, Wire, and Forgings 12Cr - 9Ni - 2Mo – 0.7Al – 0.3Ti Vacuum Induction Plus Vacuum Consumable Electrode Melted Solution Heat Treated, Precipitation Hardenable
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.