An Experimental Investigation of Two Large Annular Diffusers with Swirling and Distorted Inflow PDF Download

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An Experimental Investigation of Two Large Annular Diffusers with Swirling and Distorted Inflow

An Experimental Investigation of Two Large Annular Diffusers with Swirling and Distorted Inflow PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 112

Book Description


An Experimental Investigation of Two Large Annular Diffusers with Swirling and Distorted Inflow

An Experimental Investigation of Two Large Annular Diffusers with Swirling and Distorted Inflow PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 112

Book Description


An Experimental Investigation of Two Large Annular Diffusers with Swirling and Distorted Inflow

An Experimental Investigation of Two Large Annular Diffusers with Swirling and Distorted Inflow PDF Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Publisher:
ISBN:
Category : Diffusers
Languages : en
Pages : 103

Book Description
Two annular diffusers downstream of a nacelle-mounted fan were tested for aerodynamic performance, measured in terms of two static pressure recovery parameters (one near the diffuser exit plane and one about three diameters downstream in the settling duct) in the presence of several inflow conditions. The two diffusers each had an inlet diameter of 1.84 m, an area ratio of 2.3, and an equivalent cone angle of 11.5 deg, but were distinguished by centerbodies of different lengths. The dependence of diffuser performance on various combinations of swirling, radially distorted, and/or azimuthally distorted inflow was examined. Swirling flow and distortions in the axial velocity profile in the annulus upstream of the diffuser inlet were caused by the intrinsic flow patterns downstream of a fan in a duct and by artificial intensification of the distortions. Azimuthal distortions or defects were generated by the addition of four artificial devices (screens and fences). Pressure recover data indicated beneficial effects of both radial distortion (for a limited range of distortion levels) and inflow swirl. Small amounts of azimuthal distortion created by the artificial devices produced by only small effects on diffuser performance. A large artificial distortion device was required to produce enough azimuthal flow distortion to significantly degrade the static pressure recovery. (Author).

An Experimental Investigation of Two Large Annular Diffusers with Swirling and Distorted Inflow

An Experimental Investigation of Two Large Annular Diffusers with Swirling and Distorted Inflow PDF Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Office
Publisher:
ISBN:
Category : Diffusers
Languages : en
Pages : 112

Book Description


NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 134

Book Description


Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 212

Book Description


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Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 892

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NASA Scientific and Technical Publications PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
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Monthly Catalog of United States Government Publications PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 790

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Monthly Catalog of United States Government Publications PDF Author: United States. Superintendent of Documents
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1256

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Monthly Catalogue, United States Public Documents PDF Author:
Publisher:
ISBN:
Category : Government publications
Languages : en
Pages : 1268

Book Description