Evaluation of capillary reinforced composites /

Anti-icing of the inlet of jet engines is generally performed with high pressure heated air that is directed forward from the compressor through a series of pipes to various manifolds located near the structures to be anti-iced. From these manifolds, the air is directed to all flowpath surfaces that...

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Bibliographic Details
Main Author:	Ciardullo, Samuel W.
Corporate Authors:	General Electric Company. Aircraft Engine Business Group, Lewis Research Center
Other Authors:	Stoffer, Lewis J.
Format:	Government Document eBook
Language:	English
Published:	Cincinnati, Ohio : [Cleveland, Ohio] : General Electric Company, Aircraft Engine Business Group ; National Aeronautics and Space Administration, NASA Lewis Research Center, [1985]
Series:	NASA contractor report ; 175061.
Subjects:	Aircraft structures. Capillary flow. Composite materials. Deicing. Heat transfer. Ice formation. Intake systems. Jet engines. Laminates and Composite Materials. Thermodynamics. Snow, Ice and Permafrost. Composite structures. Capillarity. Reinforcement(structures) Deicing systems. Computer programs. Experimental data. Engine components. Air. Materials. Films. High pressure. Glass. Pipes. Coding. Ice. High strength. Mathematical analysis. Heating. Thermal conductivity. Wind tunnel tests. Accumulation. Surface temperature. Air pressure. Reinforcing materials. Jet engine inlets. Transverse. CAPILLARY REINFORCED COMPOSITES INFRARED MEASUREMENT
Online Access:	http://purl.fdlp.gov/GPO/gpo24654 http://handle.dtic.mil/100.2/ADA301939

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Call Number:		NAS 1.26:175061

NAS 1.26:175061	Available