Steady Flow Ejector Research Program PDF Download
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Author: Lockheed-Georgia Company
Publisher:
ISBN:
Category : Ejector pumps
Languages : en
Pages : 230
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Book Description
An investigation was conducted to determine the jet thrust augmentation under static conditions for rectangular parallel-divergent wall ejector configurations with multiple primary nozzles. The effect of various geometrical and flow parameters were investigated in order to provide design information. Parameters investigated included the ratio of the ejector exit area to the primary nozzle area, the diffuser angle, the mixing section length, the primary nozzle position, the entrance radius, the number of primary nozzle rows, and the primary nozzle pressure ratio and temperature ratio. The test results are generalized to obtain curves relating the augmentation factor to ejector geometry and flow parameters over a wide range of ejector exit to primary nozzle area ratios. (Author).
Author: Lockheed-Georgia Company
Publisher:
ISBN:
Category : Ejector pumps
Languages : en
Pages : 230
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Book Description
An investigation was conducted to determine the jet thrust augmentation under static conditions for rectangular parallel-divergent wall ejector configurations with multiple primary nozzles. The effect of various geometrical and flow parameters were investigated in order to provide design information. Parameters investigated included the ratio of the ejector exit area to the primary nozzle area, the diffuser angle, the mixing section length, the primary nozzle position, the entrance radius, the number of primary nozzle rows, and the primary nozzle pressure ratio and temperature ratio. The test results are generalized to obtain curves relating the augmentation factor to ejector geometry and flow parameters over a wide range of ejector exit to primary nozzle area ratios. (Author).
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 182
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Book Description
Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Military art and science
Languages : en
Pages : 1540
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Book Description
Author:
Publisher:
ISBN:
Category : Military research
Languages : en
Pages : 604
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Book Description
Author: Anjaneyulu Krothapalli
Publisher: Springer Science & Business Media
ISBN: 1461249724
Category : Science
Languages : en
Pages : 752
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Book Description
The Joint Institute for Aeronautics and Acoustics at Stanford University was established in October 1973 to provide an academic environment for long-term cooperative research between Stanford and NASA Ames Research Center. Since its establishment, the In stitute has wnducted theoretical and experimental work in the areas of aerodynamics, acoustics, fluid mechanics, flight dynamics, guid ance and control, and human factors. This research has involved Stanford faculty, research associates, graduate students, and many distinguished visitors in collaborative efforts with the research staff of NASA Ames Research Center. The occasion of the Institute's tenth anniversary was used to reflect back on where that research has brought us, and to consider where our endeavors should be directed next. Thus, an International Symposium was held to review recent advances in the fields relevant to the activities of the Institute and to discuss the areas of research to be undertaken in the future. This anniversary was also chosen a.."1 an opportunity to honor one of the Institute's founders and its di rector, Professor Krishnamurty Karamcheti. It has been his creative inspiration that has provided the ideal research environment at the Joint Institute. The International Symposium on Recent Advances in Aero dynamics and Aconstics was held at Stanford University, Stanford, California, U.S.A., August 22-26, 198:~. Thirty-five distinguished scientists were invited to present a comprehensive review on the fol lowing subject areas: unsteady aerodynamics, jets and shear layers, V /STOL aircraft aerodynamics, rotor dynamics and aerodynamics,.
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 796
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Book Description
![Unsteady Propeller Forces, Fundamental Hydrodynamics [and] Unconventional Propulsion PDF](https://books.google.com/books/content/images/frontcover/w15E1lnpCLIC?fife=w80-h100)
Author: Ralph D. Cooper
Publisher:
ISBN:
Category : Hydrodynamics
Languages : en
Pages : 1700
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Book Description
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 524
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Book Description
Author: United States. Army Research Office, Research Triangle Park, N.C.
Publisher:
ISBN:
Category : Military research
Languages : en
Pages : 156
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Book Description
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 204
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Book Description
;Contents: One-dimensional inviscid analysis of supersonic ejectors; Analysis and design method for ejector systems with second throat diffusers; The analysis of supersonic ejector systems; Ejector design for a variety of applications; Analysis of ducted mixing and burning of coaxial streams.
