Performance Characteristics of Plane-wall Two-dimensional Diffusers PDF Download

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Performance Characteristics of Plane-wall Two-dimensional Diffusers

Performance Characteristics of Plane-wall Two-dimensional Diffusers PDF Author: Elliott G. Reid
Publisher:
ISBN:
Category : Diffusers
Languages : en
Pages : 90

Book Description
Experiments have been made at Stanford University to determine the performance characteristics of plane-wall, two-dimensional diffusers which were so proportioned as to insure reasonable approximation of two-dimensional flow.

Performance Characteristics of Plane-wall Two-dimensional Diffusers

Performance Characteristics of Plane-wall Two-dimensional Diffusers PDF Author: Elliott G. Reid
Publisher:
ISBN:
Category : Diffusers
Languages : en
Pages : 90

Book Description
Experiments have been made at Stanford University to determine the performance characteristics of plane-wall, two-dimensional diffusers which were so proportioned as to insure reasonable approximation of two-dimensional flow.

Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 274

Book Description


Technical Note - National Advisory Committee for Aeronautics

Technical Note - National Advisory Committee for Aeronautics PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1160

Book Description


Discharge Coefficients for Combustor-liner Air-entry Holes

Discharge Coefficients for Combustor-liner Air-entry Holes PDF Author: Ralph T. Dittrich
Publisher:
ISBN:
Category : Combustion chambers
Languages : en
Pages : 690

Book Description
An experimental investigation was conducted to determine the effects of various geometric and flow factors on the discharge coefficients for circular holes having flow parallel to the plane of the hole. The geometric and flow factors considered were hole diameter, wall thickness at the hole, parallel-fllow duct height, boundary-layer thickness, parallel-flow velocity, static-pressure level, and pressure ratio across the test hole.

Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 796

Book Description


Separation of Flow

Separation of Flow PDF Author: Paul K. Chang
Publisher: Elsevier
ISBN: 1483181286
Category : Technology & Engineering
Languages : en
Pages : 800

Book Description
Interdisciplinary and Advanced Topics in Science and Engineering, Volume 3: Separation of Flow presents the problem of the separation of fluid flow. This book provides information covering the fields of basic physical processes, analyses, and experiments concerning flow separation. Organized into 12 chapters, this volume begins with an overview of the flow separation on the body surface as discusses in various classical examples. This text then examines the analytical and experimental results of the laminar boundary layer of steady, two-dimensional flows in the subsonic speed range. Other chapters consider the study of flow separation on the two-dimensional body, flow separation on three-dimensional body shape and particularly on bodies of revolution. This book discusses as well the analytical solutions of the unsteady flow separation. The final chapter deals with the purpose of separation flow control to raise efficiency or to enhance the performance of vehicles and fluid machineries involving various engineering applications. This book is a valuable resource for engineers.

Experimental Investigation of Attenuation of Strong Shock Waves in a Shock Tube with Hydrogen and Helium as Driver Gases

Experimental Investigation of Attenuation of Strong Shock Waves in a Shock Tube with Hydrogen and Helium as Driver Gases PDF Author: Jim J. Jones
Publisher:
ISBN:
Category : Helium
Languages : en
Pages : 716

Book Description
An experimental investigation has been made of the attenuation of strong shock waves in air in a shock tube. Time-history measurements were made of the static pressure at several stations in the wall of the tube. The internal diameter of the tube is 3.75 inches. shock-wave-velocity data were taken for a distance along the tube of about 120 feet.

List of Technical Notes, 1947-1953

List of Technical Notes, 1947-1953 PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 162

Book Description


Matrix Method for Obtaining Spanwise Moments and Deflections of Torsionally Rigid Rotor Blades with Arbitrary Loadings

Matrix Method for Obtaining Spanwise Moments and Deflections of Torsionally Rigid Rotor Blades with Arbitrary Loadings PDF Author: Alton P. Mayo
Publisher:
ISBN:
Category : Bending
Languages : en
Pages : 632

Book Description
A matrix solution for the spanwise bending moments and deflections of a torsionally rigid rotor blade subjected to an arbitrary loading is presented. The method includes the cantilever, teetering, and hinged blades in hovering and in steady forward flight. The method is comparatively short, involves only standard matrix procedures, and does not require that the mode shapes or natural frequencies be known.

A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 750

Book Description