Results 71 to 80 of about 63,038 (316)
Journal of Fluid Science and Technology, 2011 Spatial direct numerical simulation results are presented for transitional/turbulent supersonic isothermal flat plate boundary layers at M = 2.0 and impinging shock wave-boundary layer interactions.
Yusuke TOKURA, Hiroshi MAEKWA
doaj +1 more source
Molecular Oncology, EarlyView.The novel styrylquinazolinone‐based molecule W1B effectively suppresses glioblastoma by inhibiting IGF1R and EGFR. In high‐glucose microenvironments driving tumor resistance, W1B acts synergistically with the EGFR inhibitor dacomitinib. This combination safely blocks compensatory survival signaling in zebrafish xenograft models. Showcasing promising in
Patryk Rurka +9 more
wiley +1 more source
Theory and computations for breakup of unsteady subsonic or supersonic separating flows
, 1994 This study of flow just beyond a breakaway-separation point presents a description of planar nonlinear unsteady effects over a fairly wide parameter range, for a subsonic or supersonic boundary layer at large Reynolds numbers.
Vickers, IP +3 more
core +1 more source
Eliminating Boundary Layer Separation on a Cylinder with Nonuniform Suction
International Journal of Aerospace Engineering, 2020 Boundary layer separation negatively influences the performance of aerospace vehicles, for example, by triggering static stall or reducing combustion engine efficiency.
James Ramsay +2 more
doaj +1 more source
Molecular Oncology, EarlyView.Patient‐derived organoids (PDOs) from pancreatic, colorectal, and gastric cancers were used to evaluate standard and experimental therapies. Incorporating cancer‐associated fibroblasts (CAFs) into organoid cultures improved patient therapy outcome prediction.
Marcin Grochowski +12 more
wiley +1 more source
Transitional separation bubbles and unsteady aspects of aerofoil stall [PDF]
, 2008 A time-accurate solution method for the coupled potential flow and integral boundary-layer equations is used to study aerofoils near stall, where laboratory experiments have shown high-amplitude low-frequency oscillations.
Sandham, N.D.
core
Hypersonic interference heating in the vicinity of surface protuberances [PDF]
, 2010 The understanding of the behaviour of the flow around surface protuberances in hypersonic vehicles is developed and an engineering approach to predict the location and magnitude of the highest heat transfer rates in their vicinity is presented.
Garry, Kevin P. +4 more
core +1 more source
A Study on the Separation Length of Shock Wave/Turbulent Boundary Layer Interaction
International Journal of Aerospace Engineering, 2019 The separation length of shock wave/boundary layer interaction (SWBLI) was studied by a numerical method, which was validated by experimental results. The computational domain was two-dimensional (2-D).
Yong-yi Zhou, Yi-long Zhao, Yu-xin Zhao
doaj +1 more source
Effects of Surface Roughness on the Flow of High-Lift Low-Pressure Turbine
Journal of Harbin University of Science and Technology, 2019 In order to get the effects of surface roughness on turbine profile loss in different working conditions, the flow of a frontloaded blade at different incidences and different Reynolds number was analyzed in detail by numerical simulation The results ...
ZHANG Zong-chen, QIAO Wei-yang, BAI Tao
doaj +1 more source
Molecular Oncology, EarlyView.Single‐cell multi‐omics reveals epigenetic heterogeneity across therapy‐adaptive tumor states, including quiescent/dormant, drug‐tolerant persister, and EMT‐like phenotypes. By linking regulatory features with state‐associated biomarkers, these approaches inform biomarker‐guided therapeutic strategies for evolving tumors.
Hee Jung Kim +3 more
wiley +1 more source