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  • 1
    Keywords: DDC 510/.01 ; LC QA9
    Pages: Online-Ressource (vi, 113 pages)
    ISBN: 9780444533814
    Language: English
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  • 2
    Unknown
    Amsterdam : North-Holland Pub. Co
    Keywords: DDC 510/.01 ; LC QA9
    Pages: Online-Ressource (vi, 195 pages)
    ISBN: 9780444533692
    Language: English
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  • 3
    Unknown
    Amsterdam : North-Holland Pub. Co
    Keywords: DDC 510/.01 ; LC QA9
    Pages: Online-Ressource (vi, 284 pages)
    ISBN: 9780444533975
    Language: English
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  • 4
    Unknown
    Amsterdam : North-Holland Pub. Co
    Keywords: DDC 510/.01 ; LC QA9
    Pages: Online-Ressource (viii, 293 pages)
    ISBN: 9780444534071
    Language: English
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  • 5
    Unknown
    Amsterdam : North-Holland Pub. Co
    Keywords: DDC 510/.01 ; LC QA9
    Pages: Online-Ressource (v, 129 pages)
    ISBN: 9780444533838
    Language: English
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  • 6
    Publication Date: 2019-06-28
    Description: A hypervelocity impact (HVI) Whipple Shield and a method for shielding a wall from penetration by high velocity particle impacts where the Whipple Shield is comprised of spaced apart inner and outer metal sheets or walls with an intermediate cloth barrier arrangement comprised of ceramic cloth and high strength cloth which are interrelated by ballistic formulae.
    Keywords: Nonmetallic Materials
    Format: application/pdf
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  • 7
    Publication Date: 2019-06-28
    Description: One of today's most important and challenging technological problems is the development of advanced materials and processes required to design and build a fleet of supersonic High Speed Civil Transport (HSCT) airliners, a follow-up to the Concorde SST. The innovative combustor designs required for HSCT engines will need high-temperature materials with long-term environmental stability. Higher combustor liner temperatures than today's engines and the need for lightweight materials will require the use of advanced ceramic-matrix composites (CMC's) in hot-section components. The HSCT is just one example being used to demonstrate the need for such materials. This thesis evaluates silicon carbide (SiC) as a potential base material for HSCT and other similar applications. Key issues are the environmental durability for the materials of interest. One of the leading combustor design schemes leads to an environment which will contain both oxidizing and reducing gas mixtures. The concern is that these environments may affect the stability of the silica (SiO2) scale on which SiC depends for environmental protection. A unique High Pressure Burner Rig (HPBR) was developed to simulate the combustor conditions of future gas turbine engines, and a series of tests were conducted on commercially available SiC material. These tests are intended as a feasibility study for the use of these materials in applications such as the HSCT. Linear weight loss and surface recession of the SiC is observed as a result of SiO2 volatility for both fuel-lean and fuel-rich gas mixtures. These observations are compared and agree well with thermogravimetric analysis (TGA) experiments. A strong Arrhenius-type temperature dependence exists. In addition, the secondary dependencies of pressure and gas velocity are defined. As a result, a model is developed to enable extrapolation to points outside the experimental space of the burner rig, and in particular, to potential gas turbine engine conditions.
    Keywords: Nonmetallic Materials
    Type: NASA-CR-202331 , E-10685 , NAS 1.26:202331
    Format: application/pdf
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  • 8
    facet.materialart.
    Unknown
    In:  CASI
    Publication Date: 2019-06-28
    Description: Lubricating and antifoaming additives in aircraft lubricating oils may impede the escape of small bubbles from the oil by forming shells of liquid with a quasi-solid or gel structure around the bubbles. The rates of rise of small air bubbles, up to 2 millimeters in diameter, were measured at room temperature in an undoped oil, in the same oil containing foam inhibitors, and in an oil containing lubricating additives. The apparent diameter of the air bubbles was measured visually through an ocular micrometer on a traveling telescope. The bubbles in the undoped oil obeyed Stokes' Law, the rate of rise being proportional to the square of the apparent diameter and inversely proportional to the viscosity of the oil. The bubbles in the oils containing lubricating additives or foam inhibitors rose more slowly than the rate predicted by Stokes 1 Law from the apparent diameter, and the rate of rise decreased as the length of path the bubbles traveled increased. A method is derived to calculate the thickness of the liquid shell which would have to move with the bubbles in the doped oils to account for the abnoi'I!l8.lly slow velocity. The maximum thickness of this shell, calculated from the velocities observed, was equal to the bubble radius.
    Keywords: Nonmetallic Materials
    Type: NACA-TN-2033 , AD-A801536
    Format: application/pdf
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  • 9
    Publication Date: 2018-06-05
    Description: Silicon-based ceramics, such as SiC/SiC composites and Si3N4, are the prime candidates for hot section structural components of next-generation gas turbines. A key barrier to such an application is the rapid recession of silicon-based ceramics in combustion environments because of the volatilization of silica scale by water vapor (refs. 1 and 2). Environmental barrier coatings (EBC's) were developed to prevent recession in the High Speed Research--Enabling Propulsion Materials (HSR-EPM) Program (refs. 3 and 4). An investigation under the Ultra-Efficient Engine Technology Program was undertaken at the NASA Glenn Research Center to establish the upper temperature limit of the EPM EBC.
    Keywords: Nonmetallic Materials
    Type: Research and Technology 2000; NASA/TM-2001-210605
    Format: application/pdf
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  • 10
    Publication Date: 2019-07-27
    Description: Advanced environmental barrier coating concepts based on multi-component HfO2 (ZrO2) and modified mullite systems are developed for monolithic Si3N4 and SiC/SiC ceramic matrix composite (CMC) applications. Comprehensive testing approaches were established using the water vapor cyclic furnace, high pressure burner rig and laser heat flux steam rig to evaluate the coating water vapor stability, cyclic durability, radiation and erosion resistance under simulated engine environments. Test results demonstrated the feasibility and durability of the environmental barrier coating systems for 2700 to 3000 F monolithic Si3N4 and SiC/SiC CMC component applications. The high-temperature-capable environmental barrier coating systems are being further developed and optimized in collaboration with engine companies for advanced turbine engine applications.
    Keywords: Nonmetallic Materials
    Type: NASA/TM-2005-213444 , E-14980 , Third Annual Workshop on Environmental Barriwe Coatings and Enhanced Silicon Nitrides for Gas Turbines; 17-18 2004; Nashville, TN; United States
    Format: application/pdf
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