Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
Performance Characteristics of Axisymmetric Convergent-divergent Exhaust Nozzles with Longitudinal Slots in the Divergent Flaps
Author: Lawrence D. Leavitt
Publisher:
ISBN:
Category : Exhaust nozzles
Languages : en
Pages : 33
Book Description
Publisher:
ISBN:
Category : Exhaust nozzles
Languages : en
Pages : 33
Book Description
Performance Characteristics of Axisymmetric Convergent-divergent Exhaust Nozzles with Longitudinal Slots in the Divergent Flaps
Author: Lawrence D. Leavitt
Publisher:
ISBN:
Category : Exhaust nozzles
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category : Exhaust nozzles
Languages : en
Pages : 40
Book Description
Performance Characteristics of Axisymmetric Convergent-divergent Exhaust Nozzles with Longitudinal Slots in the Divergent
Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 40
Book Description
NASA Technical Paper
Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 110
Book Description
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 110
Book Description
Internal Performance Characteristics of Short Convergent-divergent Exhaust Nozzles Designed by the Method of Characteristics
Author: H. George Krull
Publisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 24
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.
Publisher:
ISBN:
Category : Charts, diagrams, etc
Languages : en
Pages : 24
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
Author: Richard J. Re
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 202
Book Description
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.
Publisher:
ISBN:
Category : Mach number
Languages : en
Pages : 202
Book Description
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
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 648
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 : 648
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
Author: Francis J. Capone
Publisher:
ISBN:
Category :
Languages : en
Pages : 276
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 276
Book Description
NASA Scientific and Technical Publications
Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 410
Book Description
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 410
Book Description
Internal Performance of a Hybrid Axisymmetric/nonaxisymmetric Convergent-divergent Nozzle
Author: John Gordon Taylor
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 64
Book Description
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 64
Book Description