Performance Characteristics of Axisymmetric Convergent-divergent Exhaust Nozzles with Longitudinal Slots in the Divergent Flaps

Performance Characteristics of Axisymmetric Convergent-divergent Exhaust Nozzles with Longitudinal Slots in the Divergent Flaps PDF Author: Lawrence D. Leavitt
Publisher:
ISBN:
Category : Exhaust nozzles
Languages : en
Pages : 33

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Performance Characteristics of Axisymmetric Convergent-divergent Exhaust Nozzles with Longitudinal Slots in the Divergent Flaps

Performance Characteristics of Axisymmetric Convergent-divergent Exhaust Nozzles with Longitudinal Slots in the Divergent Flaps PDF Author: Lawrence D. Leavitt
Publisher:
ISBN:
Category : Exhaust nozzles
Languages : en
Pages : 33

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Performance Characteristics of Axisymmetric Convergent-divergent Exhaust Nozzles with Longitudinal Slots in the Divergent Flaps

Performance Characteristics of Axisymmetric Convergent-divergent Exhaust Nozzles with Longitudinal Slots in the Divergent Flaps PDF Author: Lawrence D. Leavitt
Publisher:
ISBN:
Category : Exhaust nozzles
Languages : en
Pages : 40

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Performance Characteristics of Axisymmetric Convergent-divergent Exhaust Nozzles with Longitudinal Slots in the Divergent

Performance Characteristics of Axisymmetric Convergent-divergent Exhaust Nozzles with Longitudinal Slots in the Divergent PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 40

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NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 110

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Internal Performance Characteristics of Short Convergent-divergent Exhaust Nozzles Designed by the Method of Characteristics

Internal Performance Characteristics of Short Convergent-divergent Exhaust Nozzles Designed by the Method of Characteristics PDF Author: H. George Krull
Publisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 24

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Book Description
An evaluation of the internal performance characteristics of short nozzles designed by the method of characteristics was obtained over a range of nozzle pressure ratios from 1.5 to 22.

Isolated Performance at Mach Numbers From 0.60 to 2.86 of Several Expendable Nozzle Concepts for Supersonic Applications

Isolated Performance at Mach Numbers From 0.60 to 2.86 of Several Expendable Nozzle Concepts for Supersonic Applications PDF Author: Richard J. Re
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 202

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Investigations have been conducted in the Langley 16-Foot Transonic Tunnel (at Mach numbers from 0.60 to 1.25) and in the Langley Unitary Plan Winf Tunnel (at Mach numbers from 2.16 to 2.86) at an angle of attack of O° to determine the isolated performane of several expendable nozzle concepts for supersonic noaugmented turbojet applications. The effects of centerbody base shape, shroud length, shroud ventilation, cruciform shroud expansion ration, and cruciform shroud flap vectoring were investigated. The nozzle pressure ration range, which was a function of Mach number, was between 1.9 and 11.8 in the 16-Foot Transonic Tunnel and between 7.9 and 54.9 in the Unitary Plan WInd Tunnel. Discharge coefficient, thrust-minus-drag, and the forces and moments generated by vectoring the divergent shroud flaps (for Mach numbers of 0.60 to 1.25 only) of a cruciform nozzle configuration were measured.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 648

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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.

Static Internal Performance of a Single Expansion Ramp Nozzle with Multiaxis Thrust Vectoring Capability

Static Internal Performance of a Single Expansion Ramp Nozzle with Multiaxis Thrust Vectoring Capability PDF Author: Francis J. Capone
Publisher:
ISBN:
Category :
Languages : en
Pages : 276

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NASA Scientific and Technical Publications

NASA Scientific and Technical Publications PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 410

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Internal Performance of a Hybrid Axisymmetric/nonaxisymmetric Convergent-divergent Nozzle

Internal Performance of a Hybrid Axisymmetric/nonaxisymmetric Convergent-divergent Nozzle PDF Author: John Gordon Taylor
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 64

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