Static Internal Performance of a Nonaxisymmetric Vaned Thrust Reverser with Flow Splay Capability PDF Download

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Static Internal Performance of a Nonaxisymmetric Vaned Thrust Reverser with Flow Splay Capability

Static Internal Performance of a Nonaxisymmetric Vaned Thrust Reverser with Flow Splay Capability PDF Author: Linda S. Bangert
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 96

Book Description


Static Internal Performance of a Nonaxisymmetric Vaned Thrust Reverser with Flow Splay Capability

Static Internal Performance of a Nonaxisymmetric Vaned Thrust Reverser with Flow Splay Capability PDF Author: Linda S. Bangert
Publisher:
ISBN:
Category : Jet planes
Languages : en
Pages : 96

Book Description


Static Internal Performance of a Nonaxisymmetric Vaned Thrust Reverser with Flow Splay Capability

Static Internal Performance of a Nonaxisymmetric Vaned Thrust Reverser with Flow Splay Capability PDF Author: National Aeronautics and Space Administration (NASA)
Publisher: Createspace Independent Publishing Platform
ISBN: 9781722771300
Category :
Languages : en
Pages : 88

Book Description
An investigation was conducted in the Static Test Facility of the Langley 16-Foot Transonic Tunnel on a dual-port, nonaxisymmetric, block-and-turn type thrust reverser model with vane cascades in the reverser ports which turned the flow in the splay direction and aided in turning the flow in the reverse direction. Splaying reverser flow is a method of delaying to lower landing ground roll speeds the reingestion of hot exhaust flow into the inlets. Exhaust flow splay can also help prevent the impingement of hot exhaust gases on the empennage surfaces when the reverser is integrated into an actual airframe. The vane cascades consisted of two sets of perpendicular vanes with a variable number of turning and splay vanes. A skewed vane box was also tested which had only one set of vanes angled to provide both turning and splay. Vane cascades were designed to provide different amounts of flow splay in the top and bottom ports. Inner doors, trim tabs, and an orifice plate all provided means of varying the port area for reverser flow modulation. The outer door position was varied as a means of influencing the flow reverse angle. Nozzle pressure ratio was varied from 1.75 to approximately 6.00. Bangert, Linda S. and Leavitt, Laurence D. Langley Research Center...

Static Internal Performance of a Single-engine Nonaxisymmetric-nozzle Vaned-thrust-reverser Design with Thrust Modulation Capabilities

Static Internal Performance of a Single-engine Nonaxisymmetric-nozzle Vaned-thrust-reverser Design with Thrust Modulation Capabilities PDF Author: Laurence D. Leavitt
Publisher:
ISBN:
Category : Jet nozzles
Languages : en
Pages : 116

Book Description


NASA Technical Paper

NASA Technical Paper PDF Author:
Publisher:
ISBN:
Category : Astronautics
Languages : en
Pages : 306

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1148

Book Description


NASA Scientific and Technical Publications

NASA Scientific and Technical Publications PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 178

Book Description


Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1148

Book Description


NASA Scientific and Technical Publications

NASA Scientific and Technical Publications PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 64

Book Description


NASA SP.

NASA SP. PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 66

Book Description


Aeronautical Engineering

Aeronautical Engineering PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 188

Book Description
A selection of annotated references to unclassified reports and journal articles that were introduced into the NASA scientific and technical information system and announced in Scientific and technical aerospace reports (STAR) and International aerospace abstracts (IAA).