An Overview of Ejector Technology Development in the Air Force PDF Download
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Author: K. S. Nagaraja
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
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Book Description
In the last two decades, Air Force has made significant contributions to the development of the ejector technology for thrust augmentation purposes. Initially, Aerospace Research Laboratories at WPAFB undertook a major task of demonstrating that compact, thrust augmenting ejectors could be designed. After ARL successfully demonstrated that by utilizing hypermixing nozzles, thrust augmentation ratio of the order of two could be achieved, Flight Dynamics Laboratory launched a program of conducting preliminary design of an ejector thrust augmented demonstrator aircraft. ARL's work laid the foundation for a systematic study of the ejector application for V/STOL aircraft.
Author: K. S. Nagaraja
Publisher:
ISBN:
Category :
Languages : en
Pages : 36
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Book Description
In the last two decades, Air Force has made significant contributions to the development of the ejector technology for thrust augmentation purposes. Initially, Aerospace Research Laboratories at WPAFB undertook a major task of demonstrating that compact, thrust augmenting ejectors could be designed. After ARL successfully demonstrated that by utilizing hypermixing nozzles, thrust augmentation ratio of the order of two could be achieved, Flight Dynamics Laboratory launched a program of conducting preliminary design of an ejector thrust augmented demonstrator aircraft. ARL's work laid the foundation for a systematic study of the ejector application for V/STOL aircraft.
Author: K. A. Green
Publisher:
ISBN:
Category :
Languages : en
Pages : 7
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Book Description
During the past several years, the major ejector activity within the Navy has concentrated on the Thrust Augmentor Wing (TAW) concept and its application to the Rockwell XFV-12A technology demonstrator. Other papers to be presented in this workshop will discuss in detail the work that was accomplished during this program. The purpose of this paper is to outline some of the recent ejector technology work supported by the Naval Air Development Center jointly with the Air Force and/or NASA AMES and the rationale behind the programs.
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 324
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Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 524
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Author: R. P. Braden
Publisher:
ISBN:
Category : Short take-off and landing aircraft
Languages : en
Pages : 1094
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Author: National Research Council
Publisher: National Academies Press
ISBN: 0309061423
Category : Technology & Engineering
Languages : en
Pages : 76
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Book Description
This study was undertaken in response to a request by the U.S. Air Force that the National Research Council (NRC) examine whether the technologies that underlie the concept of a hypersonic, air-launched, air-breathing, hydrocarbon-fueled missile with speeds up to Mach 81 can be demonstrated in time to be initially operational by 2015. To conduct the study, the NRC appointed the Committee on Review and Evaluation of the Air Force Hypersonic Technology Program, under the auspices of the Air Force Science and Technology Board.
Author: Jacob Neufeld
Publisher: DIANE Publishing
ISBN: 1437912877
Category : Technology & Engineering
Languages : en
Pages : 344
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Book Description
Proceedings of a symposium co-sponsored by the Air Force Historical Foundation and the Air Force History and Museums Program. The symposium covered relevant Air Force technologies ranging from the turbo-jet revolution of the 1930s to the stealth revolution of the 1990s. Illustrations.
Author: Hugh Mitchell (CAPT, USAF., Jr)
Publisher:
ISBN:
Category : Ejector pumps
Languages : en
Pages : 56
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Book Description
Author: United States. Congress. House. Committee on Appropriations. Subcommittee on Department of Defense
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1092
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Author: United States. Congress. House. Committee on Appropriations. Subcommittee on Dept. of Defense
Publisher:
ISBN:
Category : United States
Languages : en
Pages : 1140
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Book Description
