Last edited by Nalar
Friday, August 7, 2020 | History

2 edition of Developing flow in s-shaped ducts. found in the catalog.

Developing flow in s-shaped ducts.

A. M. K. P. Taylor

Developing flow in s-shaped ducts.

by A. M. K. P. Taylor

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  • 18 Currently reading

Published by National Aeronautics and Space Administration in [s.l] .
Written in English


Edition Notes

Statement[by]A.M.K.P. Taylor, J.H. Whitelawand M. Yianneskis.
SeriesContractor reports / National Aeronautics and Space Administration -- 3759
ContributionsWhitelaw, J. H. 1936-, Yianneskis, M.
ID Numbers
Open LibraryOL13839686M

  A new method of analysis has been devised for determining the developing laminar flow and corresponding pressure drop in the entrance region of tubes and ducts. The method is formulated in a general manner which applies to ducts of any cross section. Specific application is made for flow in a circular tube and in a parallel‐plate channel, and the velocity distribution and pressure‐drop. 13–48 Development of Tables 13–49 Selecting Air Handling Units 13–54 Well Water Air Conditioning 13–54 Heat Pump/Solar Energy Application 13–54 System Description and Operation 13–60 High Velocity Dual Duct Systems 13–60 Advantages and Disadvantages 13–60 Dual Duct Cycles 13–65 Duct Sizing Technique 13–65 Large vs. Small Ducts.

Static Pressure is the pressure that causes air in the duct to: flow. Static pressure is the outward push of air against duct surfaces and is a measure of resistance when air moves through an object like duct work. Measured in inches of water column (in-wc), it acts equally in all directions and is independent of velocity. 2. Velocity pressure.   The amount of air flowing through a duct is regulated by the amount of pressure difference and by the system resistance. The higher the pressure difference, the greater the air velocity and the greater the quantity of air that will flow from the duct. Friction is a resistance which slows down airflow. The flow of air creates friction as it rubs.

Similarly the flow development within both S-shaped ducts is similar such that the circumferentially averaged profiles at duct exit are almost identical, and the operation of a downstream component would be unaffected. Overall system loss remains nominally unchanged despite the inclusion of lean and sweep and a reduction in system length.   The length of the duct is governed by the flow straightening, boundary layer development and diffusion requirments. 3D compression (Conical centrebody) For supersonic applications. Conical shockwaves from the central conical ramp are used to progressively compress the supersonic flow till a terminating normal shockwave makes the flow subsonic.


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Developing flow in s-shaped ducts by A. M. K. P. Taylor Download PDF EPUB FB2

Developing flow in S-shaped ducts. Washington, D.C.: National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va.: For sale by the National Technical Information Service], Developing flow in S-shaped ducts.

By B. Anderson, A. Taylor, J. Whitelaw and M. Yianneskis. Abstract. The velocity characteristics of laminar and turbulent developing flow in an S-duct formed from two deg bends of rectangular cross-section have been studied experimentally using laser Doppler velocimetry.

It is shown that. The velocity characteristics of laminar and turbulent developing flow in an S-duct formed from two deg bends of rectangular cross-section have been studied experimentally using laser Doppler velocimetry. It is shown that pressure-driven secondary flows arise in the first bend of the duct and reach maxima of and of the bulk velocity in the laminar and turbulent flows, by:   Measurements are presented of total pressure, static pressure, surface shear stress and yaw angle in the flow through several S-shaped ducts, each with a thin turbulent boundary layer at entry.

The results show that the region of low total pressure in the exit plane, found by previous workers, is due to expulsion of boundary-layer fluid by a Cited by:   Laser-Doppler velocimetry measured the laminar and turbulent streamwise flow in a S-duct. The wall pressure distribution and one component of cross-stream velocity were also obtained for the turbulent flow case.

Boundary layers near the duct inlet were about 25 percent of the hydraulic diameter in the laminar flow and varied around the periphery of the pipe between 10 percent and 20 Cited by:   Developing flow in S-shaped ducts. 1: Square cross-section duct Laser-Doppler velocimetry was used to measure the laminar and turbulent flow in an S-duct formed with two deg sectors of a bend with ratio of mean radius of curvature to hydraulic diameter of The boundary layers at the inlet to the bend were about 25% and 15% of the hydraulic diameter for the laminar and.

The thermal entry length solutions are available for isosceles triangular ducts with 2φ = 60 and 90° for the case of transverse velocity components, v and w, as zero for the simultaneously developing flow.

Because of the manufacturing processes employed in a heat exchanger matrix with triangular flow passages, some of the passages will have. A non-dimensional parameter ω, defined as the total pressure loss coefficient is analyzed for finding out the total pressure loss in the duct.

Cp Data obtained from the simulation of S-shaped ducts show that there is flow separation at the near side wall of the first bend and far side wall of the second bend. TECHNICAL NOTE Measurements of turbulent developing flow in a moderately curved square duct M.

Enayet, M. Gibson and M. Yianneskis* Laser-Doppler measurements in the turbulent flow in a right-angled bend of square cross-section, radius/duct-width ratioare presented and show the development of secondary circulation in cross-stream planes.

Numerical design and optimization of mechanical vane-type vortex generators in a serpentine air inlet duct 28 January | The European Physical Journal Plus, Vol.No.

2 A review of flow control techniques and optimisation in s-shaped ducts. The flows associated with these interturbine diffusers differ from those in simple annular diffusers both as a consequence of their high-curvature S-shaped geometry and of the presence of wakes created by the upstream turbine.

It is shown that even the simplest two-dimensional wakes result in significantly modified flows through such ducts. Boundary layers near the duct inlet were about 25 percent of the hydraulic diameter in the laminar flow and varied around the periphery of the pipe between 10 percent and 20 percent in turbulent flow.

Pressure-driven secondary flows develop in the first half of the S-duct and are attenuated and reversed in the second half. On swirl development in a square cross-sectioned, S-shaped duct 18 October | Experiments in Fluids, Vol. 41, No. 6 Vortex-Generator Model and Its Application to Flow Control.

The flows associated with these ducts differ from those in simple annular diffusers both as a consequence of their high-curvature S-shaped geometry and of the presence of wakes created by the upstream turbine.

where the constant C is often tabulated for a specific duct shape. Developing Laminar Flow, ReD h development of the hydrodynamic boundary layers, see Fig.

If a tube is short or. Duct System Design Guide First Edition © McGill AirFlow Corporation McGill AirFlow Corporation One Mission Park Groveport, Ohio Duct System Design i Notice: No part of this work may be reproduced or used in any form or by any Diverging-flow.

Describe procedures utilized in sheet metal development. Identify the procedures associated with joining and installing sheet metal duct.

Identify the different types of sheet metal duct systems. Identify the different types of fiberglass duct systems. State the safety regulations associated with sheet metal and fiberglass duct. Velocity characteristics of the flow in a round cross-sectional S-shaped diffusing duct with an offset of of the length (axial) of the duct were measured, using a laser Doppler anemometry and.

diameter pipe, and an S-shaped duct. The bell mouth entrance of the S-Duct is representative of inlet flow. Figure 1: ONERA S-Duct Test Apparatus. The goal of the test was to generate experimental data both with and without flow control devices as a means to validate the different turbulence models used withNavier -Stokes calculations.

Transition S-shaped intake duct is a crucial component of dual engine used in modern combat aircrafts. Present flow investigation demonstrates the flow behavior of double offset transition S-duct. HVAC Duct layout problems: Un-balanced HVAC air flow or cool air or warm air delivery due to differences in HVAC duct length, diameter, bends, restrictions may fail to properly balance air flow across a long flat building, between building floors, or where ducts have to make tortous passage from one building area to annother.Taylor AMKP, Yianneskis M,Developing flow in S-shaped ducts.

1: square cross-section duct. Laser-Doppler velocimetry was used to measure the laminar and turbulent flow in an S-duct formed with two deg sectors of a bend with ratio of mean radius of curvature to hydraulic diameter of Assuming the maximum Re for the laminar flow in a duct is Red,crit = the longest laminar developing region becomes: L e = d, i.e.

times of the tube diameter. Turbulent flow boundary layers grow faster, and the entrance region (L e) is relatively shorter.