Results 201 to 210 of about 1,247,418 (410)
Experimental Study on Abrasive Flow Polishing of Grooves and Oil Holes of Aircraft Engine Main Bearing. [PDF]
Micromachines (Basel)Zhang Q, Yu J, Wu M.
europepmc +1 more source
Hydrazine monopropellant reciprocating engine development [PDF]
A hydrazine fueled piston engine for providing 11.2 kW was developed to satisfy the need for an efficient power supply in the range from 3.7 to 74.6 kW where existing nonair-breathing power supplies such as fuel cells or turbines are inappropriate.
Akkerman, J. W.
core +1 more source
Polymer Engineering &Science, EarlyView.A model‐based strategy for the design of the emulsion polymerization recipe for a fluoroelastomer, namely Tecnoflon, is reported. This ensures target average microstructural properties like number‐average molecular weight, number of iodine end‐groups and number of bridges per chain can be obtained and preserved all along the reaction.
Luca Fois +4 more
wiley +1 more source
Fault prediction of aircraft engine based on adaptive hybrid sampling and BiLSTM. [PDF]
Sci RepHu J, Jiang X, Xu H, Zhang K.
europepmc +1 more source
Variability in airplane noise measurements [PDF]
Aircraft position and meteorological effects on accuracy of acoustic measurements for turbojet ...
Henderson, H. R., Hilton, D. A.
core +1 more source
Polymer International, EarlyView.An overview and categorization of man‐made per‐ or polyfluoroalkyl substances (PFASs) including low‐molar‐mass and high‐molar‐mass fluorochemicals, and their international regulations is presented. Though certain PFASs are toxic, bioaccumulative and cross the human cellular membranes, others, such as fluoropolymers, are safe, reliable and involved in ...
Bruno Améduri
wiley +1 more source
Robust Point Cloud Registration for Aircraft Engine Pipeline Systems. [PDF]
Sensors (Basel)Liu Y, Wang Z, Huang J, Zhang L.
europepmc +1 more source
A re-engining approach for light aircraft applied to SAFAT-03
, 2021 EBRAHIM AYOUP M. SALIH +2 more
openalex +2 more sources
Tandem Fan Applications in Advanced STOVL Fighter Configurations [PDF]
The series/parallel tandem fan engine is evaluated for application in advanced STOVL supersonic fighter aircraft. Options in engine cycle parameters and design of the front fan flow diverter are examined for their effects on engine weight, dimensions ...
Eskey, Megan A. +2 more
core +1 more source