A Parametric Study of the Air-breathing Pulsed Detonation Engine PDF Download
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Author: S. Eidelman
Publisher:
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Category :
Languages : en
Pages :
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Author: S. Eidelman
Publisher:
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Category :
Languages : en
Pages :
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Author: Hasan Zakaria Rouf
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 226
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Author: Daniel E. Paxson
Publisher:
ISBN:
Category :
Languages : en
Pages : 18
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Author: M. Champion
Publisher: Springer Science & Business Media
ISBN: 9401154325
Category : Science
Languages : en
Pages : 413
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Proceedings of the IUTAM Symposium held in Poitiers, France, 2-6 October 1995
Author: S. N. B. Murthy
Publisher: AIAA
ISBN: 9781600864216
Category : High-speed aeronautics
Languages : en
Pages : 716
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Annotation There have been impressive achievements in the last few years in the technologies associated with turboramjets and other combined cycle engines. These technologies, including their thermal management and integration with the vehicle, are the principal concerns of this volume. Drawing on the expertise of international engineers and researchers in the field of high-speed vehicle propulsion systems, these articles, written by experts from the United States, Russia, Germany, Japan, Belgium, and Israel, highlight developments in the industry.
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Languages : en
Pages : 11
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An in-house computational and experimental program to investigate and develop an air breathing pulse detonation engine (PDE) that uses a practical fuel (kerosene based, fleet-wide use, JP type) is currently underway at the Combustion Sciences Branch of the Turbine Engine Division of the Air Force Research Laboratory (AFRL/PRTS). PDE's have the potential of high thrust, low weight, low cost, high scalability, and wide operating range, but several technological hurdles must be overcome before a practical engine can be designed. This research effort involves investigating such critical issues as: detonation initiation and propagation; valving, timing and control; instrumentation and diagnostics; purging, heat transfer, and repetition rate; noise and multi-tube effects; detonation and deflagration to detonation transition modeling; and performance prediction and analysis. An innovative, four-detonation-tube engine design is currently in test and evaluation. Preliminary data are obtained with premixed hydrogen/air as the fuel/oxidizer to demonstrate proof of concept and verify models. Techniques for initiating detonations in hydrogen/air mixtures are developed without the use of oxygen enriched air. An overview of the AFRL/PRTS PDE development research program and hydrogen/air results are presented.
Author:
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Category : Airplanes
Languages : en
Pages : 640
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Author:
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Category :
Languages : en
Pages : 20
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Author:
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Category : Airplanes
Languages : en
Pages : 426
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Author: J. A. C. Kentfield
Publisher:
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Category :
Languages : en
Pages :
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