Attainable Circulation Of Airfoils In Cascade

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Attainable Circulation of Airfoils in Cascade

Author : Arthur W. Goldstein,Artur Mager
Publisher : Unknown
Page : 68 pages
File Size : 42,6 Mb
Release : 1949
Category : Aerofoils
ISBN : UOM:39015086494237

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Attainable Circulation of Airfoils in Cascade by Arthur W. Goldstein,Artur Mager Pdf

From consideration of available information on boundary-layer behaviour, a relation among profile thickness, maximum surface velocity, Reynolds number, velocity diagram, and solidity is established for a cascade of airfoils immersed in a two-dimensional incompressible fluid flow. Several cascades are computed to show the effect of various cascade design parameters on minimum required cascade solidity.

Isolated and Cascade Airfoils with Prescribed Velocity Distribution

Author : John M. Riebs,Meyer Jerison
Publisher : Unknown
Page : 56 pages
File Size : 55,9 Mb
Release : 1947
Category : Aerodynamics
ISBN : UOM:39015086493353

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Isolated and Cascade Airfoils with Prescribed Velocity Distribution by John M. Riebs,Meyer Jerison Pdf

An exact solution of the problem of designing an airfoil with a prescribed velocity distribution on the suction surface in a given uniform flow of an incompressible perfect liquid is obtained by replacing the boundary of the airfoil by vortices. By this device, a method of solution is developed, which is applicable both to isolated airfoils and to airfoils in cascade. The conformal transformation of the designed airfoil into a circle can then be obtained and the velocity distribution at any angle of attack computed. Numerical illustrations of the method are given for the airfoil in cascade.

Report - National Advisory Committee for Aeronautics

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 652 pages
File Size : 40,8 Mb
Release : 1947
Category : Aeronautics
ISBN : CORNELL:31924089884476

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Report - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Annual Report of the National Advisory Committee for Aeronautics

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 988 pages
File Size : 52,5 Mb
Release : 1949
Category : Aeronautics
ISBN : UOM:39015006372802

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Annual Report of the National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Includes the Committee's Reports no. 1-1058, reprinted in v. 1-37.

Resistance of Cascade of Airfoils in Gas Stream at Subsonic Velocity

Author : Lev Gerasimovich Loĭt︠s︡i︠a︡nskiĭ
Publisher : Unknown
Page : 38 pages
File Size : 42,8 Mb
Release : 1951
Category : Aerodynamics
ISBN : UFL:31262081062613

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Resistance of Cascade of Airfoils in Gas Stream at Subsonic Velocity by Lev Gerasimovich Loĭt︠s︡i︠a︡nskiĭ Pdf

A method of computing the resistance of a cascade of airfoils in a viscous compressible gas flow is described.

Report

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 26 pages
File Size : 52,5 Mb
Release : 1951
Category : Aeronautics
ISBN : STANFORD:36105024789500

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Report by United States. National Advisory Committee for Aeronautics Pdf

Aerodynamics of Turbines and Compressors. (HSA-1), Volume 1

Author : William R. Hawthorne
Publisher : Princeton University Press
Page : 646 pages
File Size : 46,8 Mb
Release : 2017-03-14
Category : Technology & Engineering
ISBN : 9781400885985

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Aerodynamics of Turbines and Compressors. (HSA-1), Volume 1 by William R. Hawthorne Pdf

Volume X of the High Speed Aerodynamics and Jet Propulsion series. Contents include: Theory of Two-Dimensional Flow through Cascades; Three-Dimensional Flow in Turbomachines; Experimental Techniques; Flow in Cascades; The Axial Compressor Stage; The Supersonic Compressor; Aerodynamic Design of Axial Flow Turbines; The Radial Turbine; The Centrifugal Compressor; Intermittent Flow Effects. Originally published in 1964. The Princeton Legacy Library uses the latest print-on-demand technology to again make available previously out-of-print books from the distinguished backlist of Princeton University Press. These editions preserve the original texts of these important books while presenting them in durable paperback and hardcover editions. The goal of the Princeton Legacy Library is to vastly increase access to the rich scholarly heritage found in the thousands of books published by Princeton University Press since its founding in 1905.

Stall Propagation in a Cascade of Airfoils

Author : Anthony R. Kriebel,Barry Stanley Seidel,Richard G. Schwind
Publisher : Unknown
Page : 64 pages
File Size : 40,7 Mb
Release : 1960
Category : Aerofoils
ISBN : NASA:31769000421092

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Stall Propagation in a Cascade of Airfoils by Anthony R. Kriebel,Barry Stanley Seidel,Richard G. Schwind Pdf

An experimental investigation of stall propagation in a stationary circular cascade in which high-speed schlieren and interferometer photography is used is described. This investigation suggests an analytical approach to the study of stall propagation which is valid only for an isolated blade row in an infinite flow field but which is not restricted to small unsteady perturbations or to an assumed simplified cascade geometry. Conditions necessary for the existence of the assumed type of stall cells are described and equations are derived for the velocity of stall-cell propagation.

Use of Source Distributions for Evaluating Theoretical Aerodynamics of Thin Finite Wings at Supersonic Speeds

Author : A. J. Eggers,Arthur W. Goldstein,Chung-Hua Wu,Dean R. Chapman,George J. Heimerl,Harvard Lomax,John C. Evvard,John D. Stanitz,Max. A. Heaslet,S. S. Manson,United States. National Advisory Committee for Aeronautics,Artur Mager,Gaylord O. Ellis,Lincoln Wolfestein,Loma Sluder,William M. Roberts,John R. Spreiter
Publisher : Unknown
Page : 264 pages
File Size : 46,6 Mb
Release : 1950
Category : Aerofoils
ISBN : OSU:32435063878391

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Use of Source Distributions for Evaluating Theoretical Aerodynamics of Thin Finite Wings at Supersonic Speeds by A. J. Eggers,Arthur W. Goldstein,Chung-Hua Wu,Dean R. Chapman,George J. Heimerl,Harvard Lomax,John C. Evvard,John D. Stanitz,Max. A. Heaslet,S. S. Manson,United States. National Advisory Committee for Aeronautics,Artur Mager,Gaylord O. Ellis,Lincoln Wolfestein,Loma Sluder,William M. Roberts,John R. Spreiter Pdf

Technical Note - National Advisory Committee for Aeronautics

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 1030 pages
File Size : 53,5 Mb
Release : 1958
Category : Aeronautics
ISBN : RUTGERS:39030037544717

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Technical Note - National Advisory Committee for Aeronautics by United States. National Advisory Committee for Aeronautics Pdf

Flow Through Cascades in Tandem

Author : William E. Spraglin
Publisher : Unknown
Page : 52 pages
File Size : 54,8 Mb
Release : 1951
Category : Air flow
ISBN : UOM:39015086495564

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Flow Through Cascades in Tandem by William E. Spraglin Pdf

An exact treatment of the problem of finding the incompressible, inviscid two-dimensional flow around two cascades in tandem is presented. The analysis includes solutions of both the direct and the inverse problems. These problems are solved by conformally mapping the tandem cascade onto the region between two concentric circles in which region there are suitably placed flow singularities. Formulas for the velocity and the potential in the annular region are presented in a closed form by means of elliptic functions. The equations are presented in a form suitable for computation.

NACA Research Memorandum

Author : Anonim
Publisher : Unknown
Page : 102 pages
File Size : 46,7 Mb
Release : 19??
Category : Aerodynamics
ISBN : STANFORD:36105024809647

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NACA Research Memorandum by Anonim Pdf

Two-dimensional Compressible Flow in Centrifugal Compressors with Straight Blades

Author : John D. Stanitz,Gaylord O. Ellis
Publisher : Unknown
Page : 712 pages
File Size : 49,8 Mb
Release : 1949
Category : Aeronautics
ISBN : STANFORD:36105024795754

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Two-dimensional Compressible Flow in Centrifugal Compressors with Straight Blades by John D. Stanitz,Gaylord O. Ellis Pdf

Six numerical examples are presented for steady, two-dimensional, compressible, nonviscous flow in centrifugal compressors with straight blades. A seventh example is presented for incompressible flow. The solutions also applye to radial-flow turbines with rotation and flow direction reversed. The effects of variations in following parameters were investigated: (1) flow rate, (2) impeller-tip speed, (3) variation of passage height with radius, and (4) number of blades. The numerical results are presented in plots of the streamlines, constant Mach number lines, and constant pressure-ratio lines. Correlation equations are developed whereby the flow conditions in any impeller with straight blades can be determined for all operating conditions.

Index of NACA Technical Publications

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 498 pages
File Size : 54,9 Mb
Release : 1952
Category : Aeronautics
ISBN : UCBK:C029901293

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Index of NACA Technical Publications by United States. National Advisory Committee for Aeronautics Pdf