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Learn-To-Fly Project Overview: In-Flight and Wind Tunnel Global Nonlinear Aerodynamic ModelingSummary of near real time modeling techniques applied to flight tests and wind tunnel tests.
Document ID
20200007715
Acquisition Source
Langley Research Center
Document Type
Presentation
External Source(s)
LAR-18410-1
Authors
Jay Brandon (Langley Research Center Hampton, United States)
Date Acquired
May 14, 2020
Publication Date
August 29, 2014
Publication Information
Publisher: National Aeronautics and Space Administration
Subject Category
Aircraft Design, Testing and Performance
Report/Patent Number
Report Number: NF1676L-18952
NF1676L-18952
Meeting Information
Meeting: Presentation at Boeing Commercial Aircraft Company
Location: Everett, WA
Country: US
Start Date: August 29, 2014
Sponsors: National Aeronautics and Space Administration
Funding Number(s)
WBS: 794072.02.07.06.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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