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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
20100026007
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Johnson, Wayne
(NASA Ames Research Center Moffett Field, CA, United States)
Sinsay, Jeffrey D.
(Army Research Development and Engineering Command United States)
Date Acquired
August 24, 2013
Publication Date
October 14, 2010
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
ARC-E-DAA-TN822
Report Number: ARC-E-DAA-TN822
Meeting Information
Meeting: The 3rd International Basic Research Conference on Rotorcraft Technology
Location: Nanjing, China
Country: China
Start Date: October 14, 2009
End Date: October 16, 2009
Sponsors: American Helicopter Society, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
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