Results 11 to 20 of about 782,477 (356)
Aerospace, 2023 Compression corner shock wave/boundary layer interaction (SWBLI) is a typical shock wave/boundary layer interaction (SWBLI) problem in supersonic/hypersonic flows. In previous studies, the separation flow is usually caused by a single shock wave. However,
Bo Yang +5 more
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Chemical Engineering Journal Advances, 2023 The aim of this study is to present the existence of two-dimensional steady boundary layer flow of hybrid nanofluid over a diverging channel in the occurrence of an externally applied magnetic field.
Hiranmoy Maiti, Swati Mukhopadhyay
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Three dimensional laminar boundary layer with small cross-flow [PDF]
, 1954 Important problems involving three-dimensional boundary layer occur in almost all internal and external aerodynamic configurations. For many of these, the flow outside the boundary layer may be resolved into a large principal component and a small ...
Mager, Artur
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Entropy, 2019 The hypersonic flow field around a blunt cone was simulated using a high-order finite difference method. Fast acoustic waves, slow acoustic waves, entropy waves, and vortical waves were introduced into the free-stream to determine the influence of a free-
Mingfang Shi +3 more
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Research Progress of Microjet Control of Shock Wave/Boundary Layer Interactions in Supersonic Flow Field [PDF]
Hangkong bingqi, 2022 The phenomenon of shock wave/boundary layer interaction is inevitable in the supersonic flow field. The existence of this phenomenon will have a series of adverse effects on the inner and outer flow fields of the supersonic vehicle.
Xu Hao, Du Zhaobo, Zhong Xiangyu, Huang Wei
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Some hypersonic intake studies [PDF]
, 2006 A 'two dimensional' air intake comprisipg a wedge followed by an isentropic compression has been tested in the Cranfield Gun Tunnel at Mach 8,2. These tests were performed to investigate qualitatively the intake flow starting process. The effects of cowl
Lanson, F., Stollery, J. L.
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On injection-ejection fluid influence through different accelerating porous surfaces on unsteady 2d incompressible boundary layer characteristics [PDF]
Theoretical and Applied Mechanics, 2005 Through the porous contour in perpendicular direction, the fluid of the same properties as incompressible fluid in basic flow, has been injected or ejected with velocity who is a function of the contour longitudinal coordinate and time. The corresponding
Ivanović Dečan, Ivanović Vladan
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Advances in Unsteady Boundary Layer Transition Research, Part I: Theory and Modeling
International Journal of Rotating Machinery, 2003 This two-part article presents recent advances in boundary layer research that deal with the unsteady boundary layer transition modeling and its validation.
M. T. Schobeiri, L. Wright
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Secondary instability in boundary-layer flows [PDF]
The Physics of Fluids, 1979 The stability of a secondary Tollmien–Schlichting wave, whose wavenumber and frequency are nearly one half those of a fundamental Tollmien–Schlichting instability wave, is analyzed using the method of multiple scales. Under these conditions, the fundamental wave acts as a parametric exciter for the secondary wave. The results show that the amplitude of
Nayfeh, Ali H., Bozatli, A. N.
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Heat transfer analysis of boundary layer flow
Alexandria Engineering Journal, 2016 In the present study heat transfer and entropy generation analysis of boundary layer flow of an incompressible viscous fluid over hyperbolic stretching cylinder are taken into account. The governing nonlinear partial differential equations are normalized
Abid Majeed, Tariq Javed, Irfan Mustafa
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