SUPERSONIC PROPULSION MODEL FOR USE IN AERO – PROPULSO – SERVO – ELASTIC VEHICLE DYNAMICS INVESTIGATION

SUPERSONIC PROPULSION MODEL FOR USE IN AERO – PROPULSO – SERVO – ELASTIC VEHICLE DYNAMICS INVESTIGATION

Bibliographic Details
Main Author: Connolly, Joseph W.
Language:English
Published: Case Western Reserve University School of Graduate Studies / OhioLINK 2009
Subjects:
Engineering
Supersonics
Propulsion
Aeronautics
Online Access:http://rave.ohiolink.edu/etdc/view?acc_num=case1243605610
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spelling ndltd-OhioLink-oai-etd.ohiolink.edu-case12436056102021-08-03T05:33:15Z SUPERSONIC PROPULSION MODEL FOR USE IN AERO – PROPULSO – SERVO – ELASTIC VEHICLE DYNAMICS INVESTIGATION Connolly, Joseph W. Engineering Supersonics Propulsion Aeronautics Under the NASA Fundamental Aeronautics Program the Supersonics Project aims to overcome the obstacles associated with supersonic commercial flight. The proposed vehicles are long slim body aircraft with pronounced aero-servo-elastic modes. These modes, coupled with propulsion system dynamics, can potentially lead to design challenges that influence performance characteristics such as aircraft ride quality and stability. Other disturbances upstream of the engine generated from atmospheric wind gusts, angle of attack, and yaw may also affect ride quality and stability. These design considerations can also compete with each other as well, which further complicates the development of the vehicle. To study these phenomena and their interactions an integrated model is needed that includes both airframe structural dynamics as well as the propulsion system dynamics. The focus here will be for optimal propulsion system performance, where normal inlet-engine operations are required to be closer to compressor stall and inlet unstart. This paper covers the propulsion system component modeling and controls development of an integrated mixed compression inlet and turbojet engine that will be used for a preliminary overall vehicle Aero-Propulso-Servo- Elastic model. 2009-08-03 English text Case Western Reserve University School of Graduate Studies / OhioLINK http://rave.ohiolink.edu/etdc/view?acc_num=case1243605610 http://rave.ohiolink.edu/etdc/view?acc_num=case1243605610 unrestricted This thesis or dissertation is protected by copyright: all rights reserved. It may not be copied or redistributed beyond the terms of applicable copyright laws.
collection NDLTD
language English
sources NDLTD
topic Engineering
Supersonics
Propulsion
Aeronautics
spellingShingle Engineering
Supersonics
Propulsion
Aeronautics
Connolly, Joseph W.
SUPERSONIC PROPULSION MODEL FOR USE IN AERO – PROPULSO – SERVO – ELASTIC VEHICLE DYNAMICS INVESTIGATION
author Connolly, Joseph W.
author_facet Connolly, Joseph W.
author_sort Connolly, Joseph W.
title SUPERSONIC PROPULSION MODEL FOR USE IN AERO – PROPULSO – SERVO – ELASTIC VEHICLE DYNAMICS INVESTIGATION
title_short SUPERSONIC PROPULSION MODEL FOR USE IN AERO – PROPULSO – SERVO – ELASTIC VEHICLE DYNAMICS INVESTIGATION
title_full SUPERSONIC PROPULSION MODEL FOR USE IN AERO – PROPULSO – SERVO – ELASTIC VEHICLE DYNAMICS INVESTIGATION
title_fullStr SUPERSONIC PROPULSION MODEL FOR USE IN AERO – PROPULSO – SERVO – ELASTIC VEHICLE DYNAMICS INVESTIGATION
title_full_unstemmed SUPERSONIC PROPULSION MODEL FOR USE IN AERO – PROPULSO – SERVO – ELASTIC VEHICLE DYNAMICS INVESTIGATION
title_sort supersonic propulsion model for use in aero – propulso – servo – elastic vehicle dynamics investigation
publisher Case Western Reserve University School of Graduate Studies / OhioLINK
publishDate 2009
url http://rave.ohiolink.edu/etdc/view?acc_num=case1243605610
work_keys_str_mv AT connollyjosephw supersonicpropulsionmodelforuseinaeropropulsoservoelasticvehicledynamicsinvestigation
_version_ 1719421631164579840

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