Results 21 to 30 of about 16,981 (316)

Effect of inlet and outlet flow conditions on natural gas parameters in supersonic separation process. [PDF]

PLoS ONE, 2014
A supersonic separator has been introduced to remove water vapour from natural gas. The mechanisms of the upstream and downstream influences are not well understood for various flow conditions from the wellhead and the back pipelines.
Yan Yang, Chuang Wen, Shuli Wang, Yuqing Feng   +3 more
doaj   +1 more source

Numerical research on flow field starting of supersonic compressor in outlet-opening wind tunnel

Hangkong gongcheng jinzhan
The process from test starting to supersonic flow state established in an outlet-opening wind tunnel，i. e. the starting problem of supersonic flow，has become a recognized challenge.
ZHANG Tianlong, WANG Xu, LIN Tianqi, XU Xiangshen, MU Wenpeng   +4 more
doaj   +1 more source

Supersonic micro-jet of straight micro-tube exit

Journal of Thermal Science and Technology, 2015
The experimental investigations on the phenomenon of supersonic flow at the exit of straight micro-tubes with diameters ranging from 150 to 530 μm were conducted.
Chungpyo HONG, Yasuhiro YOSHIDA, Shinichi MATSUSHITA, Ichiro UENO, Yutaka ASAKO   +4 more
doaj   +1 more source

Unsteady Supersonic Flow [PDF]

Nature, 1960
The Potential Theory of Unsteady Supersonic Flow By Prof. John W. Miles. (Cambridge Monographs on Mechanics and Applied Mathematics.) Pp. xii + 220. (Cambridge: At the University Press, 1959.) 45s. net.
openaire   +1 more source

Investigation of the Flow In Cold Condition at the Exit of a Supersonic Combustor Test Bench [PDF]

Journal of Aerospace Technology and Management, 2020
For studies of hypersonic flows and supersonic combustion in ground test facilities, three devices can be used as ram accelerators, shock tunnels and supersonic combustor test benches.
Jefte da Silva Guimarães, Valéria Serrano Faillace Oliveira Leite, Dermeval Carinhana Junior, Marco Antônio Sala Minucci   +3 more
doaj   +3 more sources

Approximate Analytical Models of Shock-Wave Structure at Steady Mach Reflection

Fluids, 2021
In this study, we obtain the comparative analysis of methods of quick approximate analytical prediction of Mach shock height in planar steady supersonic flows (for example, in supersonic jet flow and in narrowing channel between two wedges), that are ...
Mikhail V. Chernyshov, Karina E. Savelova, Anna S. Kapralova   +2 more
doaj   +1 more source

Effect of Height on the Supersonic Flow over a Blunt Vertical Fin [PDF]

Journal of Applied Fluid Mechanics
Understanding how protrusions, such as fins attached to flat or streamlined bodies, affect aerodynamics, especially in high-speed contexts, is vital for aerospace applications.
D. Sahoo, S. T. Kansara, P. Kumar
doaj   +1 more source

Exercise Interventions in Children, Adolescents and Young Adults With Paediatric Bone Tumours—A Systematic Review

Pediatric Blood &Cancer, EarlyView.
ABSTRACT Bone tumours present significant challenges for affected patients, as multimodal therapy often leads to prolonged physical limitations. This is particularly critical during childhood and adolescence, as it can negatively impact physiological development and psychosocial resilience.
Jennifer Queisser, Claire Laurie, Teresa Schmidt, Irene von Luettichau, Peter Bekkering, Sabine Kesting   +5 more
wiley   +1 more source

The anti‐CRISPR protein AcrIE8.1 inhibits the type I‐E CRISPR‐Cas system by directly binding to the Cascade subunit Cas11

FEBS Letters, EarlyView.
In this study, we present the structure of AcrIE8.1, a previously uncharacterized anti‐CRISPR protein that inhibits the type I‐E CRISPR‐Cas system. Through a combination of structural and biochemical analyses, we demonstrate that AcrIE8.1 directly binds to the Cas11 subunit of the Cascade complex to inhibit the CRISPR‐Cas system.
Young Woo Kang, Hyun Ho Park
wiley   +1 more source

Airfoil leading edge blowing to control bow shock waves

Scientific Reports, 2020
This manuscript presents a detailed characterization of active control of bow shock waves via leading edge injection, including subsonic coolant ejection and the appearance of Coanda effects.
Francisco Lozano, Guillermo Paniagua
doaj   +1 more source