Effect of Nozzle Structural Design on the Operation of the Ejector Stage with a Conical Mixing Chamber

Effect of Nozzle Structural Design on the Operation of the Ejector Stage with a Conical Mixing Chamber PDF Author: I. I. Kalmykov
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ISBN:
Category :
Languages : en
Pages : 14

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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

Effect of Nozzle Structural Design on the Operation of the Ejector Stage with a Conical Mixing Chamber PDF Author: I. I. Kalmykov
Publisher:
ISBN:
Category :
Languages : en
Pages : 14

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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

Scientific and Technical Aerospace Reports PDF Author:
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ISBN:
Category : Aeronautics
Languages : en
Pages : 970

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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

Government Reports Announcements PDF Author:
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Category : Technology
Languages : en
Pages : 1290

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Experimental Study of Zero-flow Ejectors Using Gaseous Nitrogen

Experimental Study of Zero-flow Ejectors Using Gaseous Nitrogen PDF Author: William Leroy Hill Jones
Publisher:
ISBN:
Category : Ejector pumps
Languages : en
Pages : 28

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Government Reports Announcements & Index

Government Reports Announcements & Index PDF Author:
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Category : Science
Languages : en
Pages : 248

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Effect of Convergent Ejector Nozzles on the Boattail Drag of a 16© Conical Afterbody at Mach Number of 0.6 to 1.26

Effect of Convergent Ejector Nozzles on the Boattail Drag of a 16© Conical Afterbody at Mach Number of 0.6 to 1.26 PDF Author: James M. Cubbage
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Category : Cone
Languages : en
Pages : 38

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Note on Performance of Aircraft Ejector Nozzles at High Secondary Flows

Note on Performance of Aircraft Ejector Nozzles at High Secondary Flows PDF Author: Fred D. Kochendorfer
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Category : Aeronautics
Languages : en
Pages : 26

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Effect of Nozzle Inlet Geometry on Performance of a Swiveled Convergent-divergent Nozzle

Effect of Nozzle Inlet Geometry on Performance of a Swiveled Convergent-divergent Nozzle PDF Author: Albert J. Pavli
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Category : Aerodynamics
Languages : en
Pages : 44

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International Aerospace Abstracts

International Aerospace Abstracts PDF Author:
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Category : Aeronautics
Languages : en
Pages : 940

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Applied Mechanics Reviews

Applied Mechanics Reviews PDF Author:
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Category : Mechanics, Applied
Languages : en
Pages : 636

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