EBookClubs

Read Books & Download eBooks Full Online

EBookClubs

Read Books & Download eBooks Full Online

Book An Experimental Study of a Pulsed Jet Ejector

Download or read book An Experimental Study of a Pulsed Jet Ejector written by Isaac M. Choutapalli and published by . This book was released on 2007 with total page 696 pages. Available in PDF, EPUB and Kindle. Book excerpt: The first objective was addressed by carrying out direct thrust measurements on the free steady jet, free pulsed jet and the pulsed jet ejector configurations. Within the range of parameters investigated, it has been demonstrated conclusively that for an incompressible pulsed jet (Mj = 0.30) operating at a Strouhal number of around 0.1, thrust augmentation values as high as 1.9 can be obtained with a compact ejector (L/ D ≈ 3) at an area ratio (ejector inlet area/primary nozzle exit area) of about 11.0.

Book Analytical and Experimental Study of a Pulse jet Engine

Download or read book Analytical and Experimental Study of a Pulse jet Engine written by Charles Alexander Lindley and published by . This book was released on 1949 with total page 68 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Study of a Pulse Detonation Engine Driven Ejector

Download or read book Experimental Study of a Pulse Detonation Engine Driven Ejector written by R. Shehadeh and published by . This book was released on 2003 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book An Experimental and Analytical Investigation of Pulsed jet Ejector Performance

Download or read book An Experimental and Analytical Investigation of Pulsed jet Ejector Performance written by Frederic Neal Steigman and published by . This book was released on 1969 with total page 144 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Experimental Study of Zero flow Ejectors Using Gaseous Nitrogen

Download or read book Experimental Study of Zero flow Ejectors Using Gaseous Nitrogen written by William Leroy Hill Jones and published by . This book was released on 1960 with total page 28 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Analytical and Experimental Study of the Pulsejet Ejector

Download or read book Analytical and Experimental Study of the Pulsejet Ejector written by William Stanley Johnson and published by . This book was released on 1967 with total page 248 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book Analytical and Experimental Study of the Pulsojet Ejector

Download or read book Analytical and Experimental Study of the Pulsojet Ejector written by William Stanley Johnson and published by . This book was released on 1967 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book A Simple Model of Pulsed Ejector Thrust Augmentation

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 2018-08-29 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...

Book Experimental Investigation of a Triple jet Gas Ejector

Download or read book Experimental Investigation of a Triple jet Gas Ejector written by Yu N. Vasilev and published by . This book was released on 1967 with total page 19 pages. Available in PDF, EPUB and Kindle. Book excerpt: An experimental study was made of a three-jet gas ejector in an attempt to improve ejector efficiency. The three-jet ejector consists of a converging nozzle for the high pressure gas and an annular nozzle for the low-pressure gas, and is similar to a conventional ejector; it is, however, also equipped with a tube in the center of the converging nozzle through which part of the low-pressure gas is introduced. Plots were obtained for the dependence of the compression ratio on the pressure drop in the forechamber, at various positions of the central tube, and with the converging nozzles having diameter ratios of 0.55, 0.45, and 0.35. The results showed that a compression ratio of 31 and a pressure drop of 240 can be obtained in the three-jet ejector when the outlet of the central tube is located in the minimum pressure zone. This compares very favorably with the 5.6 and 42.5 values obtained in a conventional ejector. By using a start-up control in which the central tube outlet is gradually moved into the minimum pressure zone, a compression ratio of 44 and a pressure drop of 340 can be obtained. The overall results indicate that the operation of a conventional ejector can be substantially improved by installing a central tube for the low-pressure gas. (Author).

Book An Experimental Study of Static Thrust Augmentation Using a 2 D Variable Ejector

Download or read book An Experimental Study of Static Thrust Augmentation Using a 2 D Variable Ejector written by Eli Kedem (MAJ, Israeli AF.) and published by . This book was released on 1979 with total page 162 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book An Experimental Study of a Venturi Type Air Ejector

Download or read book An Experimental Study of a Venturi Type Air Ejector written by Pradīpa Paṇḍyā and published by . This book was released on 1968 with total page 218 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book An Experimental Study of the Mixing Behaviour of Acoustically Pulsed Air Jets  microform

Download or read book An Experimental Study of the Mixing Behaviour of Acoustically Pulsed Air Jets microform written by Wai Keung Yu and published by National Library of Canada. This book was released on 1985 with total page 352 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book An Experimental Study of Circular and Rectangular Thrust Augmenting Ejectors

Download or read book An Experimental Study of Circular and Rectangular Thrust Augmenting Ejectors written by Steven G. Reznick (CAPT, USAF.) and published by . This book was released on 1980 with total page 116 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book An Experimental Study of the Draft tube Air Ejector

Download or read book An Experimental Study of the Draft tube Air Ejector written by Satish Kumar Handa and published by . This book was released on 1966 with total page 160 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Book An Experimental Study of Rectangular and Circular Thrust Augmenting Ejectors

Download or read book An Experimental Study of Rectangular and Circular Thrust Augmenting Ejectors written by Gregory Unnever (CAPT, USAF.) and published by . This book was released on 1981 with total page 132 pages. Available in PDF, EPUB and Kindle. Book excerpt: