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Rotorcraft Conceptual Design EnvironmentRequirements 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.
Document ID
20100023452
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Johnson, Wayne
(NASA Ames Research Center Moffett Field, CA, United States)
Sinsay, Jeffrey
(Army Research Development and Engineering Command United States)
Date Acquired
August 24, 2013
Publication Date
October 19, 2009
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN675
Report Number: ARC-E-DAA-TN675
Meeting Information
Meeting: 2nd International Forum on Rotorcraft Multidisciplinary Technology
Location: Seoul
Country: Korea, Republic of
Start Date: October 19, 2009
End Date: October 20, 2009
Sponsors: American Helicopter Society, Inc., Korea Aerospace Research Inst., Korean Society for Aeronautical and Space Sciences
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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