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X-29: Research AircraftA preliminary look at the Ames Dryden Flight Research Center in the context of the X-29 aircraft is provided. The uses of the X-29's 30 deg forward swept wing are examined. The video highlights the historical development of the forward swept wing, and its unique blend of speed, agility, and slow flight potential. The central optimization of the wing, the forward canard, and the rear flaps by an onboard flight computer is also described.
Document ID
19940014489
Acquisition Source
Legacy CDMS
Document Type
Video
External Source(s)
Date Acquired
August 16, 2013
Publication Date
January 1, 1991
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
ASR-237
NASA-TM-109370
NONP-NASA-VT-94-198217
Accession Number
94N18962
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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