Design and CFD Simulation of Supersonic Nozzle by Komega turbulence model for Supersonic Wind Tunnel [PDF]
E3S Web of ConferencesThis paper presents an impressive design of a convergent divergent (C-D) nozzle using the method of characteristics for a Mach number 2 test section. The nozzle’s geometry was meticulously crafted in SolidWorks, and its performance was evaluated through ...
Raman Ravi Shankar +6 more
doaj +1 more source
Closure to “Discussions of ‘Determination of Mach Number From Pressure Measurements’” (1956, Trans. ASME, 78, p. 589) [PDF]
, 1956 F. W. Barry
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Chitosan/Platelet‐Rich Plasma Implants in an Ovine Arthroscopic Model of Meniscus Repair
Journal of Orthopaedic Research, EarlyView.ABSTRACT Despite the availability of various repair techniques, many meniscal tears remain irreparable. A freeze‐dried chitosan‐based formulation reconstituted in autologous platelet‐rich plasma has shown potential in preclinical studies for enhancing suture‐based meniscus repair.
Margaux Delvaux +6 more
wiley +1 more source
Simulated flight effects on noise characteristics of a fan inlet with high throat Mach number [PDF]
An anechoic wind tunnel experiment was conducted to determine the effects of simulated flight on the noise characteristics of a high throat Mach number fan inlet.
Abbott, J. M. +2 more
core +1 more source
Nonmodal energy growth and optimal perturbations in compressible plane Couette flow
, 2008 Nonmodal transient growth studies and estimation of optimal perturbations have been made for the compressible plane Couette flow with three-dimensional disturbances.
J. Dey +3 more
core +1 more source
AMR for low Mach number reacting flow [PDF]
, 2006 We present a summary of recent progress on the development and application of adaptive mesh refinement algorithms for low Mach number reacting flows. Our approach uses a form of the low Mach number equations based on a general equation of state that discretely conserves both mass and energy.
openaire +4 more sources
Discussion: “Determination of Mach Number From Pressure Measurements” (Barry, F. W., 1956, Trans. ASME, 78, pp. 581–589) [PDF]
, 1956 W. G. Cornell
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Lipids, EarlyView.Abstract The lipid profiles of highlanders and lowlanders differ. However, studies of the lipid profiles of patients with type 2 diabetes mellitus (T2DM) living at high altitudes are limited. This study aimed to compare lipid profiles and lipoprotein particles in individuals with T2DM permanently residing in the Tibetan Plateau and those residing in ...
Chenghui Zhang +6 more
wiley +1 more source
Altitude performance of a low-noise-technology fan in a turbofan engine with and without a sound suppressing nacelle [PDF]
Test variables were inlet Reynolds number index (0.2 to 0.5), flight Mach number (0.2 to 0.8), and flow distortion (tip radial and combined circumferential - tip radial patterns). Results are limited to fan bypass and overall engine performance.
Abdelwahah, M. +2 more
core +1 more source
Combustion and Propulsion: High Mach Number Air-Breathing Engines [PDF]
, 1960 W. Cawood
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