Symposium on Boundary Layer Effects in AerodynamicsAircraft Engineering & Aerospace Technology
The aim of this work is to introduce, review and discuss similarity and pseudosimilarity solutions to a class of problems in the boundary layer theory. The boundary layer technique is encountered in many aspects of fluid dynamics and aerodynamics. This technique has been created for finding the ...
Assessment of boundary layer flow modeling approaches in computational fluid dynamics for compressible external aerodynamics using naca- 64618 airfoil-shankaramurthy.H.M, Madhukeshwara.N,Shankaramurthy.H.M,International journal of innovative research in science, engineering and technology,vol 1,pgno:6,...
In the study of supersonic and hypersonic problems, shock wave/boundary layer interaction is one of the most common complex flow phenomena. These complex phenomena can significantly affect the aerodynamics and thermodynamics of aerospace vehicles. An accurate understanding of their dynamics can contribute...
Book2017, Aerodynamics for Engineering Students (Seventh Edition) E.L. Houghton, ... Daniel T. Valentine Explore book 3.2 Boundary-Layer Theory Here we discuss ideas for simplifying the NS equations to come up with Prandtl's boundary-layer equations. We begin by considering the boundary layer ...
, Cooling by protective fluid films, in High Speed Aerodynamics and Jet Propulsion, Vol. 5 Sec. G, Turbulent Flows and Heat Transfer, Princeton Univ. Press 1959. Low, G. M. (1955) The compressible laminar boundary layer with fluid injection. NACA, Washington (D.C.) Maddox, A. R. (...
boundary layer interaction Abdellah Hadjadj · Jean-Paul Dussauge Published online: 26 November 2009 © Springer-Verlag 2009 1 Introduction Shock wave boundary layer interaction (SWBLI) in high- speed aerodynamics has been the subject of several exper- imental and numerical studies in the past. ...
Bernoullis equation It is valid just outside Boundary Layer, where between two points (1,2) on the flow stream (1) Since pressure in the boundary layer is same on y axis and that just outside, the expression for pressure gradient along x is also valid inside the boundary layer. Navier...
Book2013, Aerodynamics for Engineering Students (Sixth Edition) E.L. Houghton, ... Daniel T. Valentine Explore book 2.12.2 Boundary-Layer Thickness for Laminar and Turbulent Flows In this section we will examine the thickness of the boundary layer along a flat plate. This flow is illustrated ...
This property can be applied to a lot of known self-similar motions. Some examples are considered for which the final form of the boundary layer equations is formulated.This is a preview of subscription content, log in via an institution to check access. ...