Approximate Design Method For High Solidity Blade Elements In Compressors And Turbines

Author : John Stanitz
Publisher : Рипол Классик
Page : 79 pages
File Size : 54,8 Mb
Release : 1951
Category : History
ISBN : 9785881585655

Get Book

Approximate design method for high-solidity blade elements in compressors and turbines by John Stanitz Pdf

An approximate blade-element design method is developed for compressible or incompressible nonviscous flow in high-solidity stators or rotors of axial-, radial-, or mixed-flow compressors, turbines, or two-dimensinal cascades. The method is based upon channel-type flow between blade elements on a specified surface of revolution that lies between the hub and shroud (casing) and is concentric with the axis of the compressor turbine. The blade elements is designed for prescribed velocities along the blade-element profile as a function of distance along meridonal lines on the surface of revolution. Two numerical examples are presented: (1) the design of a blade-element profile for a plane two-dimensional cascade in compressible flow with the prescribed velocities along the profiles; and (2) the design of a blade element for the impeller of a mixed-flow centrifugal compressor.

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 1026 pages
File Size : 52,6 Mb
Release : 1955
Category : Aeronautics
ISBN : RUTGERS:39030037542810

Get Book

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

Author : John D. Stanitz,Leonard J. Sheldrake
Publisher : Unknown
Page : 72 pages
File Size : 41,5 Mb
Release : 1952
Category : Aeronautics
ISBN : UOM:39015086495788

Get Book

Application of a Channel Design Method to High-solidity Cascades and Tests of an Impulse Cascade with 90° of Turning by John D. Stanitz,Leonard J. Sheldrake Pdf

A technique is developed for the application of a channel design method to the design of high-solidity cascades with prescribed velocity distributions as a function of arc length along the blade-element profile. The technique applies to both incompressible and subsonic linearized compressible (ratio of specific heats equal to -1.0), nonviscous, irrotational, fluid motion. An impulse cascade with 90 degree turning was designed for incompressible flow and was tested at the design angle of attack over a range of downstream Mach number from 0.2 to choke flow. To achieve good efficiency, the cascade was designed for prescribed velocities with maximum allowable blade loading according to limitations imposed by considerations of boundary-layer separation.

Author : Anonim
Publisher : Unknown
Page : 606 pages
File Size : 50,6 Mb
Release : 1951
Category : Aeronautics
ISBN : UIUC:30112008553916

Get Book

Technical Note by Anonim Pdf

Author : Ernest Franklin Fiock,Carl Halpern
Publisher : Unknown
Page : 120 pages
File Size : 52,9 Mb
Release : 1954
Category : Gas-turbines
ISBN : UIUC:30112106781815

Get Book

Bibliography of Books and Published Reports on Gas Turbines, Jet Propulsion and Rocket Power Plants by Ernest Franklin Fiock,Carl Halpern Pdf

Author : Anonim
Publisher : Unknown
Page : 122 pages
File Size : 49,7 Mb
Release : 1954
Category : Electronic
ISBN : MINN:31951000628866T

Get Book

National Bureau of Standards Circular by Anonim Pdf

Author : Anonim
Publisher : Unknown
Page : 122 pages
File Size : 55,7 Mb
Release : 1954
Category : Weights and measures
ISBN : UOM:39015024251558

Get Book

Circular of the Bureau of Standards by Anonim Pdf

Author : Anonim
Publisher : Unknown
Page : 750 pages
File Size : 41,9 Mb
Release : 1949
Category : Aeronautics
ISBN : UVA:X004173285

Get Book

A Selected Listing of NASA Scientific and Technical Reports for ... by Anonim Pdf

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 388 pages
File Size : 54,7 Mb
Release : 1959
Category : Aeronautics
ISBN : UCBK:C029901327

Get Book

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

Author : William R. Hawthorne
Publisher : Princeton University Press
Page : 646 pages
File Size : 40,8 Mb
Release : 2017-03-14
Category : Technology & Engineering
ISBN : 9781400885985

Get Book

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.

Author : United States. National Advisory Committee for Aeronautics
Publisher : Unknown
Page : 568 pages
File Size : 42,5 Mb
Release : 1951
Category : Aeronautics
ISBN : IND:30000088900174

Get Book

Research Abstracts by United States. National Advisory Committee for Aeronautics Pdf

Author : Anonim
Publisher : Unknown
Page : 488 pages
File Size : 49,7 Mb
Release : 1958
Category : Aerodynamics
ISBN : STANFORD:36105024809746

Get Book

NACA Research Memorandum by Anonim Pdf

Author : B. Lakshminarayana,Werner R. Britsch,Walter S. Gearhart
Publisher : Unknown
Page : 450 pages
File Size : 54,6 Mb
Release : 1974
Category : Fluid mechanics
ISBN : STANFORD:36105113767755

Get Book

Fluid Mechanics, Acoustics, and Design of Turbomachinery by B. Lakshminarayana,Werner R. Britsch,Walter S. Gearhart Pdf

Author : Robert O. Bullock
Publisher : Unknown
Page : 552 pages
File Size : 45,5 Mb
Release : 1965
Category : Axial flow compressors
ISBN : NASA:31769000652464

Get Book

Aerodynamic Design of Axial Flow Compressors by Robert O. Bullock Pdf

Author : Lewis Research Center
Publisher : Unknown
Page : 542 pages
File Size : 43,6 Mb
Release : 1965
Category : Axial flow compressors
ISBN : STANFORD:36105113764901

Get Book

Aerodynamic Design of Axial-flow Compressors by Lewis Research Center Pdf