FRINK Linked Data Fragments server

Matches in SemOpenAlex for { <https://semopenalex.org/work/W2959647612> ?p ?o ?g. }

• W2959647612 abstract "Conceptual design is often considered to be the most important step in the design of a new product or the modification of an existing product. The important steps in this conceptual design phase is the synthesis of potential solutions into concepts, the evaluation of these concepts within a repeatable and robust design methodology framework and analysis to identify and characterise the preferred solution concept. This research has arisen from problems associated with developing aircraft-based design modification concepts and predicting the impact of these changes as they propagate or flow down through the various aircraft subsystems, impacting engineering design, and leading to certification and operations challenges. This research problem is particularly evident in highly integrated systems such as high-performance military aircraft, helicopters, and complex civil aircraft. To illustrate this methodology the author has selected two case studies which apply two different alternate propulsion system technologies to small aircraft. These case studies were selected to provide a diverse design modification space encompassing differing aircraft roles and mission types, differing technologies and subsystems integration scope, and different data sources collection and analysis methods.In order to combine the elements of design synthesis, evaluation of concept alternatives and analysis of outputs, this thesis has formulated a matrix-based conceptual design methodology. This methodology extends current knowledge by implementing the concepts of design synthesis, evaluation and analysis as an iterative process, and building and linking together existing techniques. This new methodology combined various techniques and methods such as Quality Function Deployment (QFD), quantified morphological matrices (QMM), Pugh’s decision matrices, change options Multiple-Domain Matrices (MDM), and has adapted the Change Propagation Method (CPM).The second extension to current knowledge in this area was the development of Engineering and Certification Domain Mapping Matrix (DMM) techniques based on Design Structure Matrices (DSM). This extension into engineering and certification domain was undertaken to ensure that important modification-related risks and costs were incorporated into the early stages of design. The extension adopted existing DSM and DMM-based techniques and tools to evaluate the impact of changes to subsystems and hence impact of risks and costs resulting from aircraft modifications using change propagation method analysis techniques.The validation of this conceptual design methodology was achieved by verifying and assessing the adequacy of its application through an analysis process which examined (1) coverage of the design space attributes; (2) validation of the methodology against accepted scientific and industry conceptual design frameworks; and (3) confirmation of the existing techniques, structures and tools applied within the methodology." @default.
• W2959647612 created "2019-07-23" @default.
• W2959647612 creator A5070657199 @default.
• W2959647612 date "2019-01-01" @default.
• W2959647612 modified "2023-09-27" @default.
• W2959647612 title "A conceptual design methodology for evaluation of alternate propulsion system modifications on small aircraft" @default.
• W2959647612 hasPublicationYear "2019" @default.
• W2959647612 type Work @default.
• W2959647612 sameAs 2959647612 @default.
• W2959647612 citedByCount "0" @default.
• W2959647612 crossrefType "dissertation" @default.
• W2959647612 hasAuthorship W2959647612A5070657199 @default.
• W2959647612 hasConcept C1034443 @default.
• W2959647612 hasConcept C106246047 @default.
• W2959647612 hasConcept C111919701 @default.
• W2959647612 hasConcept C120208923 @default.
• W2959647612 hasConcept C127413603 @default.
• W2959647612 hasConcept C146978453 @default.
• W2959647612 hasConcept C199360897 @default.
• W2959647612 hasConcept C201995342 @default.
• W2959647612 hasConcept C21547014 @default.
• W2959647612 hasConcept C2778012447 @default.
• W2959647612 hasConcept C2778648169 @default.
• W2959647612 hasConcept C34972735 @default.
• W2959647612 hasConcept C41008148 @default.
• W2959647612 hasConcept C42360764 @default.
• W2959647612 hasConcept C539667460 @default.
• W2959647612 hasConcept C71822192 @default.
• W2959647612 hasConcept C78519656 @default.
• W2959647612 hasConcept C86992474 @default.
• W2959647612 hasConcept C98045186 @default.
• W2959647612 hasConceptScore W2959647612C1034443 @default.
• W2959647612 hasConceptScore W2959647612C106246047 @default.
• W2959647612 hasConceptScore W2959647612C111919701 @default.
• W2959647612 hasConceptScore W2959647612C120208923 @default.
• W2959647612 hasConceptScore W2959647612C127413603 @default.
• W2959647612 hasConceptScore W2959647612C146978453 @default.
• W2959647612 hasConceptScore W2959647612C199360897 @default.
• W2959647612 hasConceptScore W2959647612C201995342 @default.
• W2959647612 hasConceptScore W2959647612C21547014 @default.
• W2959647612 hasConceptScore W2959647612C2778012447 @default.
• W2959647612 hasConceptScore W2959647612C2778648169 @default.
• W2959647612 hasConceptScore W2959647612C34972735 @default.
• W2959647612 hasConceptScore W2959647612C41008148 @default.
• W2959647612 hasConceptScore W2959647612C42360764 @default.
• W2959647612 hasConceptScore W2959647612C539667460 @default.
• W2959647612 hasConceptScore W2959647612C71822192 @default.
• W2959647612 hasConceptScore W2959647612C78519656 @default.
• W2959647612 hasConceptScore W2959647612C86992474 @default.
• W2959647612 hasConceptScore W2959647612C98045186 @default.
• W2959647612 hasLocation W29596476121 @default.
• W2959647612 hasOpenAccess W2959647612 @default.
• W2959647612 hasPrimaryLocation W29596476121 @default.
• W2959647612 hasRelatedWork W1537660933 @default.
• W2959647612 hasRelatedWork W1968877027 @default.
• W2959647612 hasRelatedWork W1990015990 @default.
• W2959647612 hasRelatedWork W2082935627 @default.
• W2959647612 hasRelatedWork W2153230475 @default.
• W2959647612 hasRelatedWork W2208210079 @default.
• W2959647612 hasRelatedWork W2213867230 @default.
• W2959647612 hasRelatedWork W2519258528 @default.
• W2959647612 hasRelatedWork W2739032036 @default.
• W2959647612 hasRelatedWork W2801090100 @default.
• W2959647612 hasRelatedWork W2891409699 @default.
• W2959647612 hasRelatedWork W2944113599 @default.
• W2959647612 hasRelatedWork W2973299887 @default.
• W2959647612 hasRelatedWork W3034379213 @default.
• W2959647612 hasRelatedWork W3034984089 @default.
• W2959647612 hasRelatedWork W311723942 @default.
• W2959647612 hasRelatedWork W3161526324 @default.
• W2959647612 hasRelatedWork W3172782696 @default.
• W2959647612 hasRelatedWork W3193151188 @default.
• W2959647612 hasRelatedWork W48147891 @default.
• W2959647612 isParatext "false" @default.
• W2959647612 isRetracted "false" @default.
• W2959647612 magId "2959647612" @default.
• W2959647612 workType "dissertation" @default.