Comparison of NACA 65-series Compressor-blade Pressure Distributions and Performance in a Rotor and in Cascade

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ISBN 13 :
Total Pages : 60 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Comparison of NACA 65-series Compressor-blade Pressure Distributions and Performance in a Rotor and in Cascade by : Willard R. Westphal

Download or read book Comparison of NACA 65-series Compressor-blade Pressure Distributions and Performance in a Rotor and in Cascade written by Willard R. Westphal and published by . This book was released on 1951 with total page 60 pages. Available in PDF, EPUB and Kindle. Book excerpt: The comparison indicated that cascade data accurately predicted the turning angle and blade pressure distribution obtained in the compressor at design conditions. At other than design angle of attack, large differences, probably due to secondary flows, were observed near the inner casing.

NACA 65-series Compressor Rotor Performance with Varying Annulus-area Ratio, Solidity, Blade Angle, and Reynolds Number and Comparison with Cascade Results

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ISBN 13 :
Total Pages : 66 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis NACA 65-series Compressor Rotor Performance with Varying Annulus-area Ratio, Solidity, Blade Angle, and Reynolds Number and Comparison with Cascade Results by : Wallace M. Schulze

Download or read book NACA 65-series Compressor Rotor Performance with Varying Annulus-area Ratio, Solidity, Blade Angle, and Reynolds Number and Comparison with Cascade Results written by Wallace M. Schulze and published by . This book was released on 1953 with total page 66 pages. Available in PDF, EPUB and Kindle. Book excerpt: A typical axial-flow compressor rotor using NACA 65-series compressor blades was tested at low speeds and its performance was measured over a range of quantity flow rates at several values of annulus-area ratio, blade-setting angle, solidity, and Reynolds number to compare with porouswall cascade results. The data obtained using varying annulus area were corrected to the two-dimensional-flow condition by two methods.

Technical Note - National Advisory Committee for Aeronautics

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ISBN 13 :
Total Pages : 1136 pages
Book Rating : 4.E/5 ( download)

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Book Synopsis Technical Note - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Technical Note - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1958 with total page 1136 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Note

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ISBN 13 :
Total Pages : 622 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Technical Note by :

Download or read book Technical Note written by and published by . This book was released on 1957 with total page 622 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Noise Survey of a Full-scale Supersonic Turbine-driven Propeller Under Static Conditions

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ISBN 13 :
Total Pages : 742 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Noise Survey of a Full-scale Supersonic Turbine-driven Propeller Under Static Conditions by : Max C. Kurbjun

Download or read book Noise Survey of a Full-scale Supersonic Turbine-driven Propeller Under Static Conditions written by Max C. Kurbjun and published by . This book was released on 1957 with total page 742 pages. Available in PDF, EPUB and Kindle. Book excerpt: Overall sound-pressure levels and frequency spectra of the noise emitted from a full-scale, 7.2-foot-diameter, 3, 500 rpm, three-blade, supersonic propeller mounted on a turbine-powered airplane have been obtained under static conditions at stations about the propeller at a 100-foot radius.

Annual Report - National Advisory Committee for Aeronautics

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

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Book Synopsis Annual Report - National Advisory Committee for Aeronautics by : United States. National Advisory Committee for Aeronautics

Download or read book Annual Report - National Advisory Committee for Aeronautics written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1957 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes the Committee's Technical reports no. 1-1058, reprinted in v. 1-37.

Research Abstracts and Reclassification Notice

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ISBN 13 :
Total Pages : 508 pages
Book Rating : 4.3/5 ( download)

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

Download or read book Research Abstracts and Reclassification Notice written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1954 with total page 508 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Applied Mechanics Reviews

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ISBN 13 :
Total Pages : 636 pages
Book Rating : 4.:/5 (26 download)

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Book Synopsis Applied Mechanics Reviews by :

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1973 with total page 636 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Band-pass Shock and Vibration Absorbers for Application to Aircraft Landing Gear

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

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Book Synopsis Band-pass Shock and Vibration Absorbers for Application to Aircraft Landing Gear by : Emanuel Schnitzer

Download or read book Band-pass Shock and Vibration Absorbers for Application to Aircraft Landing Gear written by Emanuel Schnitzer and published by . This book was released on 1956 with total page 652 pages. Available in PDF, EPUB and Kindle. Book excerpt: A new class of frequency-selective shock absorbers called band-pass shock absorbers which were conceived as a means of overcoming some of the limitations of conventional shock absorbers is described. These shock absorber designs are introduced, special emphasis being given to their use in landing and taxiing problems of high-speed aircraft. For such aircraft operated on rough land or water runways, conventional oleo struts approach a rigid condition for bum[s with steep slopes and thereby develop and transmit severe shock loads to the aircraft fuselage. The operation of the band-pass shock absorbers in the reduction of loads in certain selected frequency ranges is described. Theoretical equations are derived and solutions are made for several cases for the purpose of comparing the low-pass and conventional shock-absorber actions. The results indicate that the band-pass shock absorbers should alleviate high-frequency or rapidly applied impact loads but should retain the characteristics of conventional oleo struts when taxiing and design landing loads are slowly applied. A number of variations in design are presented for low-pass shock absorbers and reference is made to double-acting band-pass vibration absorbers for other applications.

Index of NACA Technical Publications

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ISBN 13 :
Total Pages : 580 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 1956 with total page 580 pages. Available in PDF, EPUB and Kindle. Book excerpt:

NASA Reference Publication

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ISBN 13 :
Total Pages : 944 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis NASA Reference Publication by :

Download or read book NASA Reference Publication written by and published by . This book was released on 1977 with total page 944 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 : 818 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 1954 with total page 818 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Analysis of Aerodynamic Blade-loading-limit Parameters for NACA 65-(C[sub Zeta]0A10) 10 Compressor-blade Sections at Low Speeds

Download Analysis of Aerodynamic Blade-loading-limit Parameters for NACA 65-(C[sub Zeta]0A10) 10 Compressor-blade Sections at Low Speeds PDF Online Free

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

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Book Synopsis Analysis of Aerodynamic Blade-loading-limit Parameters for NACA 65-(C[sub Zeta]0A10) 10 Compressor-blade Sections at Low Speeds by : Melvyn Savage

Download or read book Analysis of Aerodynamic Blade-loading-limit Parameters for NACA 65-(C[sub Zeta]0A10) 10 Compressor-blade Sections at Low Speeds written by Melvyn Savage and published by . This book was released on 1955 with total page 38 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Report

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ISBN 13 :
Total Pages : 94 pages
Book Rating : 4.F/5 ( download)

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

Download or read book Report written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1958 with total page 94 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 : 647 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 647 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.

Report

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ISBN 13 :
Total Pages : 1138 pages
Book Rating : 4.:/5 (319 download)

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Book Synopsis Report by :

Download or read book Report written by and published by . This book was released on 1958 with total page 1138 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Aerodynamic Design of Axial-flow Compressors

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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: