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Rotorcraft conceptual design environment
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Johnson, Wayne Sinsay, Jeffrey D. |
| Copyright Year | 2010 |
| Description | Requirements for a rotorcraft conceptual design environment are discussed, from the perspective of a government laboratory. Rotorcraft design work in a government laboratory must support research, by producing technology impact assessments and defining the context for research and development; and must support the acquisition process, including capability assessments and quantitative evaluation of designs, concepts, and alternatives. An information manager that will enable increased fidelity of analysis early in the design effort is described. This manager will be a framework to organize information that describes the aircraft, and enable movement of that information to and from analyses. Finally, a recently developed rotorcraft system analysis tool is described. |
| File Size | 1335382 |
| Page Count | 9 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20100026007 |
| Archival Resource Key | ark:/13960/t0jt4nd56 |
| Language | English |
| Publisher Date | 2010-10-14 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Design, Testing And Performance Impact Damage Assessment Systems Analysis Rotary Wing Aircraft Design Analysis Technology Assessment Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
