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AFC-Enabled Vertical Tail System Integration StudyThis document serves as the final report for the SMAAART AFC-Enabled Vertical Tail System Integration Study. Included are the ground rule assumptions which have gone into the study, layouts of the baseline and AFC-enabled configurations, critical sizing information, system requirements and architectures, and assumed system properties that result in an NPV assessment of the two candidate AFC technologies.
Document ID
20140003900
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Mooney, Helen P.
(Boeing Co. Huntington Beach, CA, United States)
Brandt, John B.
(Boeing Co. Huntington Beach, CA, United States)
Lacy, Douglas S.
(Boeing Co. Huntington Beach, CA, United States)
Whalen, Edward A.
(Boeing Co. Huntington Beach, CA, United States)
Date Acquired
April 28, 2014
Publication Date
March 1, 2014
Subject Category
Aerodynamics
Report/Patent Number
NF1676L-18162
NASA/CR-2014-218168
Funding Number(s)
CONTRACT_GRANT: NNL10AA05B
WBS: WBS 699959.02.07.07.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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