Author: I. I. Kalmykov
Publisher:
ISBN:
Category :
Languages : en
Pages : 14
Book Description
The optimum configuration of a supersonic propelling nozzle for an air driven two stage ejector is selected experimentally. The nozzles tested were of the conical type with inlets and outlets of various design and with various lengths of the cylindrical portion of the throat. Nozzles with various expansion ratios were also tested. The nozzles were placed in the plane of the inlet section, along the axis, of a 5 degree conical mixing chamber (of the first stage). An analysis of the results indicated that an underexpanded mode of operation is optimum for the ejector nozzle. (Author).
Effect of Nozzle Structural Design on the Operation of the Ejector Stage with a Conical Mixing Chamber
Author: I. I. Kalmykov
Publisher:
ISBN:
Category :
Languages : en
Pages : 14
Book Description
The optimum configuration of a supersonic propelling nozzle for an air driven two stage ejector is selected experimentally. The nozzles tested were of the conical type with inlets and outlets of various design and with various lengths of the cylindrical portion of the throat. Nozzles with various expansion ratios were also tested. The nozzles were placed in the plane of the inlet section, along the axis, of a 5 degree conical mixing chamber (of the first stage). An analysis of the results indicated that an underexpanded mode of operation is optimum for the ejector nozzle. (Author).
Publisher:
ISBN:
Category :
Languages : en
Pages : 14
Book Description
The optimum configuration of a supersonic propelling nozzle for an air driven two stage ejector is selected experimentally. The nozzles tested were of the conical type with inlets and outlets of various design and with various lengths of the cylindrical portion of the throat. Nozzles with various expansion ratios were also tested. The nozzles were placed in the plane of the inlet section, along the axis, of a 5 degree conical mixing chamber (of the first stage). An analysis of the results indicated that an underexpanded mode of operation is optimum for the ejector nozzle. (Author).
Scientific and Technical Aerospace Reports
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 970
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 : 970
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.
Government Reports Announcements
Author:
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 1290
Book Description
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 1290
Book Description
Experimental Study of Zero-flow Ejectors Using Gaseous Nitrogen
Author: William Leroy Hill Jones
Publisher:
ISBN:
Category : Ejector pumps
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category : Ejector pumps
Languages : en
Pages : 28
Book Description
Government Reports Announcements & Index
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 248
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 248
Book Description
Effect of Convergent Ejector Nozzles on the Boattail Drag of a 16© Conical Afterbody at Mach Number of 0.6 to 1.26
Author: James M. Cubbage
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 38
Book Description
Publisher:
ISBN:
Category : Cone
Languages : en
Pages : 38
Book Description
Note on Performance of Aircraft Ejector Nozzles at High Secondary Flows
Author: Fred D. Kochendorfer
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 26
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 26
Book Description
Effect of Nozzle Inlet Geometry on Performance of a Swiveled Convergent-divergent Nozzle
Author: Albert J. Pavli
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 44
Book Description
International Aerospace Abstracts
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 940
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 940
Book Description
Applied Mechanics Reviews
Author:
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 636
Book Description
Publisher:
ISBN:
Category : Mechanics, Applied
Languages : en
Pages : 636
Book Description