Investigation of an Impulse Axial-flow Compressor

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Publisher :
ISBN 13 :
Total Pages : 56 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Investigation of an Impulse Axial-flow Compressor by : John R. Erwin

Download or read book Investigation of an Impulse Axial-flow Compressor written by John R. Erwin and published by . This book was released on 1950 with total page 56 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation of an Impulse Axial-flow Compressor Rotor Over a Range of Blade Angles

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Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Investigation of an Impulse Axial-flow Compressor Rotor Over a Range of Blade Angles by : Wallace M. Schulze

Download or read book Investigation of an Impulse Axial-flow Compressor Rotor Over a Range of Blade Angles written by Wallace M. Schulze and published by . This book was released on 1950 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Design of Axial-flow Compressors

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Publisher :
ISBN 13 :
Total Pages : 542 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Aerodynamic Design of Axial-flow Compressors by : Lewis Research Center

Download or read book Aerodynamic Design of Axial-flow Compressors written by Lewis Research Center and published by . This book was released on 1965 with total page 542 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Axial-flow Compressors

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Publisher : American Society of Mechanical Engineers
ISBN 13 :
Total Pages : 386 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Axial-flow Compressors by : Ronald H. Aungier

Download or read book Axial-flow Compressors written by Ronald H. Aungier and published by American Society of Mechanical Engineers. This book was released on 2003 with total page 386 pages. Available in PDF, EPUB and Kindle. Book excerpt: This book provides a thorough description of an aerodynamic design and analysis systems for Axial-Flow Compressors. It describes the basic fluid dynamic and thermodynamic principles, empirical models and numerical methods used for the full range of procedures and analytical tools that an engineer needs for virtually any tupe of Axial-Flow Compressor, aerodynamic design or analysis activity. It reviews and evaluates several design strategies that have been recommended in the literature or which have been found to be effective. It gives a complete description of an actual working system, such that readers can implement all or part of the system. Engineers responsible for developing, maintaining of improving design and analysis systems can benefit greatly from this type of reference. The technology has become so complex and the role of computers so pervasive that about the only way this can be done today is to concentrate on a specific design and analysis system. The author provides practical methodology as well as the details needed to implement the suggested procedures.

NACA Research Memorandum

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ISBN 13 :
Total Pages : 102 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis NACA Research Memorandum by :

Download or read book NACA Research Memorandum written by and published by . This book was released on 19?? with total page 102 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

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Publisher : Princeton University Press
ISBN 13 : 1400885981
Total Pages : 646 pages
Book Rating : 4.4/5 (8 download)

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

Download or read book Aerodynamics of Turbines and Compressors. (HSA-1), Volume 1 written by William R. Hawthorne and published by Princeton University Press. This book was released on 2017-03-14 with total page 646 pages. Available in PDF, EPUB and Kindle. Book excerpt: 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.

An Investigation of the Dynamic Characteristics of Axial Flow Compressors

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Publisher :
ISBN 13 :
Total Pages : 0 pages
Book Rating : 4.:/5 (142 download)

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Book Synopsis An Investigation of the Dynamic Characteristics of Axial Flow Compressors by : Guo-Cai Tang

Download or read book An Investigation of the Dynamic Characteristics of Axial Flow Compressors written by Guo-Cai Tang and published by . This book was released on 1990 with total page 0 pages. Available in PDF, EPUB and Kindle. Book excerpt: This paper reports an experimental investigation of the dynamic behavior of an axial flow compressor when the flow rate if forced to vary quickly. The results are discussed in two aspects: general trends and special points. Generally, there is a deviation of the dynamic characteristic from the steady-state one, depending upon the algebraic sum of the inertial effect and the lag effect. For the present axial flow compressor, lightly-loaded, the dynamic characteristic goes above the steady-state one while closing the valve and below the steady-state one for opening the valve. Physical explanation is given to the general trend and also to the difference between the behavior of the axial flow compressor and that of the centrifugal compressor. Specifically, the rapid closing of the valve will end up with an operating point end dynamic breaking into the instability limit while the throttle setting is somewhat away from the instability limit position for steady-state operation; and the rapid opening of the valve may produce an initial transient decrease in flow rate thus may have an initial dynamic breaking into the instability limit. Physical explanation is also given to these two special points, which are of great engineering interest with regard to the instability issue.

National Bureau of Standards Circular

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Publisher :
ISBN 13 :
Total Pages : 122 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis National Bureau of Standards Circular by :

Download or read book National Bureau of Standards Circular written by and published by . This book was released on 1954 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Bibliography of Books and Published Reports on Gas Turbines, Jet Propulsion and Rocket Power Plants

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Publisher :
ISBN 13 :
Total Pages : 120 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Bibliography of Books and Published Reports on Gas Turbines, Jet Propulsion and Rocket Power Plants by : Ernest Franklin Fiock

Download or read book Bibliography of Books and Published Reports on Gas Turbines, Jet Propulsion and Rocket Power Plants written by Ernest Franklin Fiock and published by . This book was released on 1954 with total page 120 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Research Abstracts

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ISBN 13 :
Total Pages : 568 pages
Book Rating : 4.3/5 ( download)

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Book Synopsis Research Abstracts by : United States. National Advisory Committee for Aeronautics

Download or read book Research Abstracts written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Circular of the Bureau of Standards

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Publisher :
ISBN 13 :
Total Pages : 122 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Circular of the Bureau of Standards by :

Download or read book Circular of the Bureau of Standards written by and published by . This book was released on 1954 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Index of NACA Technical Publications

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Publisher :
ISBN 13 :
Total Pages : 388 pages
Book Rating : 4.:/5 (2 download)

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Book Synopsis Index of NACA Technical Publications by : United States. National Advisory Committee for Aeronautics

Download or read book Index of NACA Technical Publications written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1959 with total page 388 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Design of Axial Flow Compressors

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Publisher :
ISBN 13 :
Total Pages : 552 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Aerodynamic Design of Axial Flow Compressors by : Robert O. Bullock

Download or read book Aerodynamic Design of Axial Flow Compressors written by Robert O. Bullock and published by . This book was released on 1965 with total page 552 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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

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Publisher :
ISBN 13 :
Total Pages : 750 pages
Book Rating : 4.X/5 (4 download)

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Book Synopsis A Selected Listing of NASA Scientific and Technical Reports for ... by :

Download or read book A Selected Listing of NASA Scientific and Technical Reports for ... written by and published by . This book was released on 1949 with total page 750 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Flutter Analysis of Rectangular Wings of Very Low Aspect Ratio

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ISBN 13 :
Total Pages : 652 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Flutter Analysis of Rectangular Wings of Very Low Aspect Ratio by : Robert William Fralich

Download or read book Flutter Analysis of Rectangular Wings of Very Low Aspect Ratio written by Robert William Fralich and published by . This book was released on 1958 with total page 652 pages. Available in PDF, EPUB and Kindle. Book excerpt: A flutter analysis, employing slender-body aerodynamic theory and thin-plate theory, is made for rectangular wings of very low aspect ratio with a constant thickness. The spanwise variation of wing deflection is assumed to be given by a parabola, and the chordwise variation is allowed complete freedom. The results show the vsriation of flutter speed and male shape with aspect ratio. Comparisons are made with additional resuits obtained by approximating the chordwise deflection shape by use of parabolic or cubic curves. The analysis shows that the cubic approximation gives good resuits for a ratio of chord to semispan less than 3.

Performance of Supersonic Axial-flow Compressors Based on One-dimensional Analysis

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ISBN 13 :
Total Pages : 34 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Performance of Supersonic Axial-flow Compressors Based on One-dimensional Analysis by : Linwood C. Wright

Download or read book Performance of Supersonic Axial-flow Compressors Based on One-dimensional Analysis written by Linwood C. Wright and published by . This book was released on 1949 with total page 34 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of an Axial-flow Supersonic Compressor Having Sharp Leading-edge Blades with an 8-percent Mean Thickness-chord Ratio

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Publisher :
ISBN 13 :
Total Pages : 38 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Experimental Investigation of an Axial-flow Supersonic Compressor Having Sharp Leading-edge Blades with an 8-percent Mean Thickness-chord Ratio by : Theodore J. Goldberg

Download or read book Experimental Investigation of an Axial-flow Supersonic Compressor Having Sharp Leading-edge Blades with an 8-percent Mean Thickness-chord Ratio written by Theodore J. Goldberg and published by . This book was released on 1955 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt: