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A Simple Model Of Pulsed Ejector Thrust Augmentation
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Book Synopsis A Simple Model of Pulsed Ejector Thrust Augmentation by :
Download or read book A Simple Model of Pulsed Ejector Thrust Augmentation written by and published by . This book was released on 2003 with total page 32 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Author :National Aeronautics and Space Administration (NASA) Publisher :Createspace Independent Publishing Platform ISBN 13 :9781720364979 Total Pages :30 pages Book Rating :4.3/5 (649 download)
Book Synopsis A Simple Model of Pulsed Ejector Thrust Augmentation by : National Aeronautics and Space Administration (NASA)
Download or read book A Simple Model of Pulsed Ejector Thrust Augmentation written by National Aeronautics and Space Administration (NASA) and published by Createspace Independent Publishing Platform. This book was released on 2018-05-29 with total page 30 pages. Available in PDF, EPUB and Kindle. Book excerpt: A simple model of thrust augmentation from a pulsed source is described. In the model it is assumed that the flow into the ejector is quasi-steady, and can be calculated using potential flow techniques. The velocity of the flow is related to the speed of the starting vortex ring formed by the jet. The vortex ring properties are obtained from the slug model, knowing the jet diameter, speed and slug length. The model, when combined with experimental results, predicts an optimum ejector radius for thrust augmentation. Data on pulsed ejector performance for comparison with the model was obtained using a shrouded Hartmann-Sprenger tube as the pulsed jet source. A statistical experiment, in which ejector length, diameter, and nose radius were independent parameters, was performed at four different frequencies. These frequencies corresponded to four different slug length to diameter ratios, two below cut-off, and two above. Comparison of the model with the experimental data showed reasonable agreement. Maximum pulsed thrust augmentation is shown to occur for a pulsed source with slug length to diameter ratio equal to the cut-off value.Wilson, Jack and Deloof, Richard L. (Technical Monitor)Glenn Research CenterTHRUST AUGMENTATION; MATHEMATICAL MODELS; FLOW VELOCITY; HARTMANN-SPRENGER TUBES; VORTEX RINGS; PULSED JET ENGINES; EJECTORS
Download or read book Research & Technology 2003 written by and published by DIANE Publishing. This book was released on with total page 264 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis AIAA Aerospace Sciences Meeting and Exhibit, 42nd by :
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Book Synopsis Workshop on Thrust Augmenting Ejectors by :
Download or read book Workshop on Thrust Augmenting Ejectors written by and published by . This book was released on 1979 with total page 524 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis AIAA Journal by : American Institute of Aeronautics and Astronautics
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Book Synopsis Scientific and Technical Aerospace Reports by :
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Download or read book Research & Technology 2002 written by and published by DIANE Publishing. This book was released on with total page 274 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Pulse Reactor Lift-propulsion System Development Program by : Raymond Marshall Lockwood
Download or read book Pulse Reactor Lift-propulsion System Development Program written by Raymond Marshall Lockwood and published by . This book was released on 1963 with total page 344 pages. Available in PDF, EPUB and Kindle. Book excerpt: The Pulse Reactor Engine Program is aimed at developing efficient, high performance lift-propulsion systems that have no moving parts. The Pulse Reactor engine is unique in that it rejects foreign particles that are denser than air; therefore, it can operate in the interface between ground and air that is denied to other aircraft lift-propulsion systems. In particular, development has been concerned with the performance effects of (1) engine size, (2) new shapes, (3) forward flight and vertical flight performance, (4) engine controls and accessories, (5) pulse reactor materials, construction techniques and engine durability.
Book Synopsis Navy Research Task Summary by : United States. Office of Naval Research
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Book Synopsis Navy Research Task Summary, 1961 by : United States. Office of Naval Research
Download or read book Navy Research Task Summary, 1961 written by United States. Office of Naval Research and published by . This book was released on 1962 with total page 378 pages. Available in PDF, EPUB and Kindle. Book excerpt:
Book Synopsis Official Gazette of the United States Patent and Trademark Office by : United States. Patent and Trademark Office
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Book Synopsis 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit 10-13 July 2005, Tucson, Arizona: 05-3800 - 05-3849 by :
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Book Synopsis 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit July 20-23, 2003, Huntsville, Alabama: 03-4950 - 03-4999 by :
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Book Synopsis Proceedings of the Second Symposium on Jet Pumps & Ejectors and Gas Lift Techniques, 1975, Cambridge by :
Download or read book Proceedings of the Second Symposium on Jet Pumps & Ejectors and Gas Lift Techniques, 1975, Cambridge written by and published by . This book was released on 1975 with total page 404 pages. Available in PDF, EPUB and Kindle. Book excerpt: