Results 161 to 170 of about 238,845 (361)
Discussion: “Problems Encountered in the Translation of Compressor Performance From One Gas to Another” (Hartmann, M. J., and Wilcox, W. W., 1957, Trans. ASME, 79, pp. 887–897) [PDF]
Joseph T Hamrick
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By fabricating and covalently assembling gelatin methacryloyl (GelMA) porous microgels, a new class of granular hydrogel scaffolds with hierarchical porosity is developed. These scaffolds have a significantly higher void fraction than their counterparts made up of nonporous microgels, enhancing cell recruitment and tissue integration. This research may
Alexander Kedzierski+9 more
wiley +1 more source
Study of blade aspect ratio on a compressor front stage aerodynamic and mechanical design report [PDF]
A single stage compressor was designed with the intent of demonstrating that, for a tip speed and hub-tip ratio typical of an advanced core compressor front stage, the use of low aspect ratio can permit high levels of blade loading to be achieved at an ...
Burger, G. D., Lee, D., Snow, D. W.
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Instability and Surge in Dual Entry Centrifugal Compressors [PDF]
J. L. Dussourd, William G. Putman
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Wearable Haptic Feedback Interfaces for Augmenting Human Touch
The wearable haptic feedback interfaces enhance user experience in gaming, social media, biomedical instrumentation, and robotics by generating tactile sensations. This review discusses and categorizes current haptic feedback interfaces into force, thermal, and electrotactile stimulation‐based haptic feedback interfaces, elucidating their current ...
Shubham Patel+3 more
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On Performance Characteristics of a Centrifugal Compressor with Supersonic Impeller Tip Speed
Ichiro Watanabe
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Experimental Noise Studies of Inlet Guide Vane-Rotor-Stator Interactions for a Single-Stage Axial-Flow Compressor [PDF]
John L Crigler, W. L. Copeland
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The fabrication of a cellularized, multilayered 3D printed cylindrical model comprising hybrid bioinks inspired by the natural extracellular environment as an approach to artery mimetics, is presented. Using embedded bioprinting, interlayer crosslinking of self‐supporting concentric cylinders is achieved.
Uxue Aizarna‐Lopetegui+7 more
wiley +1 more source
A turbojet simulator for Mach numbers up to 2.0 [PDF]
A turbojet simulator was designed and fabricated for use in wind tunnel models. The simulator contains a six-stage, axial-flow compressor powered by a three-stage, axial-flow turbine. High pressure heated air was used to drive the turbine.
Nosek, S. M.+3 more
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Theoretical Researches on Axial-Flow Compressors (Part III))
Takefumi IKUI, Kashiku TODA
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