Title:
Technology Infusion and Resource Allocation for a Civil Tiltrotor

dc.contributor.author Mavris, Dimitri N. en_US
dc.contributor.author Baker, Andrew Paul en_US
dc.contributor.author Schrage, Daniel P. en_US
dc.contributor.corporatename American Helicopter Society
dc.date.accessioned 2005-05-26T14:04:33Z
dc.date.available 2005-05-26T14:04:33Z
dc.date.issued 2000-01 en_US
dc.description Proceedings of the AHS Vertical Lift Aircraft Design Conference, San Francisco, CA, January 19-21, 2000. en_US
dc.description.abstract The methodology presented in this paper is concerned with the ability to make informed decisions early in the design time line in order to provide a feasible, viable and robust system to the customer. Increasingly, the issues of affordability, uncertainty in design and technology impact assessment are shaping the modern design environment. Current methodologies and techniques are not able to properly handle these issues. The research presented here builds on the authors?previous work which described an appropriate probabilistic design environment that allows for design in the presence of uncertainty as well as the infusion and assessment of new technologies. This environment is an essential part of a design methodology referred to as the Technology Identification, Evaluation and Selection (TIES) method. The objective of this research is to provide a comprehensive, structured, and robust methodology for decision making in the early phases of rotorcraft design. In this paper the authors will describe in detail the steps that encompass the TIES methodology. Illustrative examples of techniques, methods and tools used during the methodology will be presented as applied to NASA? Short Haul Civil Tiltrotor. en_US
dc.format.extent 128523 bytes
dc.format.mimetype application/pdf
dc.identifier.uri http://hdl.handle.net/1853/6394
dc.language.iso en_US en_US
dc.publisher Georgia Institute of Technology en_US
dc.publisher Georgia Institute of Technology
dc.publisher.original American Helicopter Society (AHS)
dc.relation.ispartofseries ASDL; AHS-2000-01-AB en_US
dc.relation.ispartofseries ASDL; AHS-2000-01-AB
dc.subject Tilt rotor aircraft en_US
dc.subject Decision-making en_US
dc.subject Early phases of design en_US
dc.subject Feasibility/viability assessment method en_US
dc.subject Robust design simulations en_US
dc.subject Affordability en_US
dc.subject Modeling of uncertainty en_US
dc.subject Technological impact en_US
dc.subject Probabilistic design en_US
dc.subject Technology identification, evaluation and selection en_US
dc.subject Rotorcraft design en_US
dc.title Technology Infusion and Resource Allocation for a Civil Tiltrotor en_US
dc.type Text
dc.type.genre Paper
dspace.entity.type Publication
local.contributor.author Mavris, Dimitri N.
local.contributor.corporatename Daniel Guggenheim School of Aerospace Engineering
local.contributor.corporatename Aerospace Systems Design Laboratory (ASDL)
local.contributor.corporatename College of Engineering
relation.isAuthorOfPublication d355c865-c3df-4bfe-8328-24541ea04f62
relation.isOrgUnitOfPublication a348b767-ea7e-4789-af1f-1f1d5925fb65
relation.isOrgUnitOfPublication a8736075-ffb0-4c28-aa40-2160181ead8c
relation.isOrgUnitOfPublication 7c022d60-21d5-497c-b552-95e489a06569
Files
Original bundle
Now showing 1 - 1 of 1
Thumbnail Image
Name:
AHS-2000-01-AB.pdf
Size:
125.51 KB
Format:
Adobe Portable Document Format
Description: