An Experimental Investigation of Ultrashort Annular Convergent Nozzles for Operation in the Sub-critical and Low Super-critical Pressure Ratio Regime

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ISBN 13 :
Total Pages : 294 pages
Book Rating : 4.:/5 (38 download)

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Book Synopsis An Experimental Investigation of Ultrashort Annular Convergent Nozzles for Operation in the Sub-critical and Low Super-critical Pressure Ratio Regime by : William Frederick Vossman

Download or read book An Experimental Investigation of Ultrashort Annular Convergent Nozzles for Operation in the Sub-critical and Low Super-critical Pressure Ratio Regime written by William Frederick Vossman and published by . This book was released on 1965 with total page 294 pages. Available in PDF, EPUB and Kindle. Book excerpt:

On the Losses in Convergent Nozzles

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ISBN 13 :
Total Pages : 94 pages
Book Rating : 4.:/5 (7 download)

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Book Synopsis On the Losses in Convergent Nozzles by : Alexander L. Mellanby

Download or read book On the Losses in Convergent Nozzles written by Alexander L. Mellanby and published by . This book was released on 1921 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Annular Internal-external-expansion Rocket Nozzles for Large Booster Applications

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ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Annular Internal-external-expansion Rocket Nozzles for Large Booster Applications by : James F. Connors

Download or read book Annular Internal-external-expansion Rocket Nozzles for Large Booster Applications written by James F. Connors and published by . This book was released on 1961 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of Shock-cell Noise Reduction for Single-stream Nozzles in Simulated Flight

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ISBN 13 :
Total Pages : 406 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Experimental Investigation of Shock-cell Noise Reduction for Single-stream Nozzles in Simulated Flight by :

Download or read book Experimental Investigation of Shock-cell Noise Reduction for Single-stream Nozzles in Simulated Flight written by and published by . This book was released on 1984 with total page 406 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Experimental Investigation of Shock-cell Noise Reduction for Single Stream Nozzles in Simulated Flight

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ISBN 13 :
Total Pages : 404 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Experimental Investigation of Shock-cell Noise Reduction for Single Stream Nozzles in Simulated Flight by : K. Yamamoto

Download or read book Experimental Investigation of Shock-cell Noise Reduction for Single Stream Nozzles in Simulated Flight written by K. Yamamoto and published by . This book was released on 1984 with total page 404 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Internal Performance Characteristics of Short Convergent-divergent Exhaust Nozzles Designed by the Method of Characteristics

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ISBN 13 :
Total Pages : 24 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Internal Performance Characteristics of Short Convergent-divergent Exhaust Nozzles Designed by the Method of Characteristics by : H. George Krull

Download or read book Internal Performance Characteristics of Short Convergent-divergent Exhaust Nozzles Designed by the Method of Characteristics written by H. George Krull and published by . This book was released on 1956 with total page 24 pages. Available in PDF, EPUB and Kindle. Book excerpt: An evaluation of the internal performance characteristics of short nozzles designed by the method of characteristics was obtained over a range of nozzle pressure ratios from 1.5 to 22.

Effect of Geometric Parameters on the Static Performance of an Annular Nozzle with a Concave Central Base

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ISBN 13 :
Total Pages : 1 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Effect of Geometric Parameters on the Static Performance of an Annular Nozzle with a Concave Central Base by : Charles E. Mercer

Download or read book Effect of Geometric Parameters on the Static Performance of an Annular Nozzle with a Concave Central Base written by Charles E. Mercer and published by . This book was released on 1962 with total page 1 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental investigation of annular convergent nozzles with concave central bases was conducted. The effects of variation in the ratio of annulus-gap width to base radius and the ratio of annulus-gap width to base depth were examined. Thrust performance comparable to that of a conventional convergent nozzle was obtained for those configurations in which the ratio of annulus-gap width to base radius was largest, that is, approximately 0.25. In general, increasing the base depth by extending the turning lip improved thrust performance and increased pressures on the base. (Author).

Experimental Investigation of Shock-cell Noise Reduction for Dual-stream Nozzles in Simulated Flight

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ISBN 13 :
Total Pages : 198 pages
Book Rating : 4.F/5 ( download)

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Book Synopsis Experimental Investigation of Shock-cell Noise Reduction for Dual-stream Nozzles in Simulated Flight by :

Download or read book Experimental Investigation of Shock-cell Noise Reduction for Dual-stream Nozzles in Simulated Flight written by and published by . This book was released on 1984 with total page 198 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Static Thrust of an Annular Nozzle with a Concave Central Base

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ISBN 13 :
Total Pages : 22 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Static Thrust of an Annular Nozzle with a Concave Central Base by : Blake W. Corson (Jr)

Download or read book Static Thrust of an Annular Nozzle with a Concave Central Base written by Blake W. Corson (Jr) and published by . This book was released on 1960 with total page 22 pages. Available in PDF, EPUB and Kindle. Book excerpt: A static test of an annular nozzle with a concave central base, producing a jet in which tangents to the jet streamlines at the exit converged toward a region on the axis of symmetry downstream of the exit, has indicated good thrust performance. A value of nozzle-flow coefficient only slightly less than unity indicates the internal loss to be small. Pressures on the concave central base are relatively large and positive, and a predictable portion of the total thrust of the jet is exerted on the central base.

Experimental Investigation of Shock-cell Noise Reduction for Dual-stream Nozzles in Simulated Flight

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ISBN 13 :
Total Pages : 196 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis Experimental Investigation of Shock-cell Noise Reduction for Dual-stream Nozzles in Simulated Flight by : B. A. Janardan

Download or read book Experimental Investigation of Shock-cell Noise Reduction for Dual-stream Nozzles in Simulated Flight written by B. A. Janardan and published by . This book was released on 1984 with total page 196 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Approximate Theoretical Method for Modeling the Static Thrust Performance of Non-axisymmetric Two-dimensional Convergent-divergent Nozzles

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ISBN 13 :
Total Pages : 54 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis An Approximate Theoretical Method for Modeling the Static Thrust Performance of Non-axisymmetric Two-dimensional Convergent-divergent Nozzles by :

Download or read book An Approximate Theoretical Method for Modeling the Static Thrust Performance of Non-axisymmetric Two-dimensional Convergent-divergent Nozzles written by and published by . This book was released on 1995 with total page 54 pages. Available in PDF, EPUB and Kindle. Book excerpt:

On the Losses in Convergent Nozzles (Classic Reprint)

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Publisher : Forgotten Books
ISBN 13 : 9780484584876
Total Pages : 94 pages
Book Rating : 4.5/5 (848 download)

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Book Synopsis On the Losses in Convergent Nozzles (Classic Reprint) by : A. L. Mellanby

Download or read book On the Losses in Convergent Nozzles (Classic Reprint) written by A. L. Mellanby and published by Forgotten Books. This book was released on 2017-12-23 with total page 94 pages. Available in PDF, EPUB and Kindle. Book excerpt: Excerpt from On the Losses in Convergent Nozzles In illustration, Fig. 1 gives a few such curves and, while it indicates differences between the various experimental results, it shows very clearly the peculiarity referred to. The curves for saturated steam flow in straight convergent nozzles show the feature of excessive discharge by rising to values above unity towards the critical range; but, even with this effect, the curve forms are of the same general type as for superheated Steam, where such an influence is absent. About the Publisher Forgotten Books publishes hundreds of thousands of rare and classic books. Find more at www.forgottenbooks.com This book is a reproduction of an important historical work. Forgotten Books uses state-of-the-art technology to digitally reconstruct the work, preserving the original format whilst repairing imperfections present in the aged copy. In rare cases, an imperfection in the original, such as a blemish or missing page, may be replicated in our edition. We do, however, repair the vast majority of imperfections successfully; any imperfections that remain are intentionally left to preserve the state of such historical works.

An Experimental Investigation of Thrust Vectoring Two-dimensional Convergent-divergent Nozzles Installed in a Twin-engine Fighter Model at High Angles of Attack

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ISBN 13 :
Total Pages : 128 pages
Book Rating : 4.:/5 (317 download)

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Book Synopsis An Experimental Investigation of Thrust Vectoring Two-dimensional Convergent-divergent Nozzles Installed in a Twin-engine Fighter Model at High Angles of Attack by :

Download or read book An Experimental Investigation of Thrust Vectoring Two-dimensional Convergent-divergent Nozzles Installed in a Twin-engine Fighter Model at High Angles of Attack written by and published by . This book was released on 1990 with total page 128 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Theoretical and Experimental Investigation of the Angularity Loss for Short Convergent-divergent Nozzles with Small Expansion Ratios

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (377 download)

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Book Synopsis A Theoretical and Experimental Investigation of the Angularity Loss for Short Convergent-divergent Nozzles with Small Expansion Ratios by : Daniel John Lahti

Download or read book A Theoretical and Experimental Investigation of the Angularity Loss for Short Convergent-divergent Nozzles with Small Expansion Ratios written by Daniel John Lahti and published by . This book was released on 1970 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Investigation of Installation Effects on Single-engine Convergent-divergent Nozzles

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ISBN 13 :
Total Pages : 244 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Investigation of Installation Effects on Single-engine Convergent-divergent Nozzles by : James R. Burley

Download or read book Investigation of Installation Effects on Single-engine Convergent-divergent Nozzles written by James R. Burley and published by . This book was released on 1982 with total page 244 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Experimental Investigation of the Critical Flow of Air-water Mixtures Through a Vertical, Two-dimensional, Converging-diverging Nozzle

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (41 download)

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Book Synopsis An Experimental Investigation of the Critical Flow of Air-water Mixtures Through a Vertical, Two-dimensional, Converging-diverging Nozzle by : James F. Muir

Download or read book An Experimental Investigation of the Critical Flow of Air-water Mixtures Through a Vertical, Two-dimensional, Converging-diverging Nozzle written by James F. Muir and published by . This book was released on 1970 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Analytical and Experimental Investigation of Annular Propulsive Nozzles

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ISBN 13 :
Total Pages : 37 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Analytical and Experimental Investigation of Annular Propulsive Nozzles by :

Download or read book Analytical and Experimental Investigation of Annular Propulsive Nozzles written by and published by . This book was released on 1993 with total page 37 pages. Available in PDF, EPUB and Kindle. Book excerpt: The final report consists of AIAA papers. The report presents an analytical performance prediction methodology for annular propulsion nozzles with and without swirl introduced in the combustor upstream of the nozzle. Four types of swirlers were investigated: free vortex, constant angle, forced vortex and Rankine vortex swirlers. For the no-swirl case thrust efficiencies and static pressure profiles from cold flow testing of selected nozzles are summarized and compared to the predictions ... Ramjets, Supersonics.