Author: A. M. Abdel-Fattah
Publisher:
ISBN: 9780642108364
Category : Airplanes
Languages : en
Pages : 5
Book Description
The results of theoretical assessment of two stage thrust augmenting ejectors are presented and compared with those of single stage ejectors. The mixing ducts were of constant cross sectional area, the flows at the inlet and exit planes of each stage were assumed to be uniform, and friction effects were ignored. It was found that staging the ejector increases thrust augmentation at all primary jet stagnation pressures, but is more effective in the low pressure range and with high ejector area ratios for any gas combination. With a Hot Rocket-Air combination, the benefit of staging is much less than with an unheated Air-Air combination, and does not appear to be of practical use.
A Theoretical Study of Two Stage Thrust Augmenting Ejectors
Author: A. M. Abdel-Fattah
Publisher:
ISBN: 9780642108364
Category : Airplanes
Languages : en
Pages : 5
Book Description
The results of theoretical assessment of two stage thrust augmenting ejectors are presented and compared with those of single stage ejectors. The mixing ducts were of constant cross sectional area, the flows at the inlet and exit planes of each stage were assumed to be uniform, and friction effects were ignored. It was found that staging the ejector increases thrust augmentation at all primary jet stagnation pressures, but is more effective in the low pressure range and with high ejector area ratios for any gas combination. With a Hot Rocket-Air combination, the benefit of staging is much less than with an unheated Air-Air combination, and does not appear to be of practical use.
Publisher:
ISBN: 9780642108364
Category : Airplanes
Languages : en
Pages : 5
Book Description
The results of theoretical assessment of two stage thrust augmenting ejectors are presented and compared with those of single stage ejectors. The mixing ducts were of constant cross sectional area, the flows at the inlet and exit planes of each stage were assumed to be uniform, and friction effects were ignored. It was found that staging the ejector increases thrust augmentation at all primary jet stagnation pressures, but is more effective in the low pressure range and with high ejector area ratios for any gas combination. With a Hot Rocket-Air combination, the benefit of staging is much less than with an unheated Air-Air combination, and does not appear to be of practical use.
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1460
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1460
Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.
Workshop on Thrust Augmenting Ejectors
Author:
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 524
Book Description
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 524
Book Description
Applied Mechanics Reviews
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 770
Book Description
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 770
Book Description
A Selected Listing of NASA Scientific and Technical Reports for ...
Author: United States. National Aeronautics and Space Administration. Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1680
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1680
Book Description
NASA Scientific and Technical Reports
Author: United States. National Aeronautics and Space Administration Scientific and Technical Information Division
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1440
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1440
Book Description
Technical Abstract Bulletin
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 914
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 914
Book Description
Proceedings of the ASME-JSME Thermal Engineering Joint Conference
Author:
Publisher:
ISBN:
Category : Heat engineering
Languages : en
Pages : 542
Book Description
Publisher:
ISBN:
Category : Heat engineering
Languages : en
Pages : 542
Book Description
Technical Publications Announcements with Indexes
Author: United States. National Aeronautics and Space Administration
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 796
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 796
Book Description
Report
Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 32
Book Description