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The XFV-12A Thrust-Augmented Wing (TAW) prototype aircraftThe XFV-12A, a unique V/STOL technology prototype aircraft being developed for the Navy, is described. The innovative design features a thrust augmented wing and a canard ejector. Structural, functional, and control test performances are discussed. Static tether test results are also discussed. Assessment of test results are given along with projections for future modification areas.
Document ID
19800001894
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Murphy, R. (Naval Air Systems Command Washington, DC, United States)
Lewis, E. L. (Naval Air Systems Command Washington, DC, United States)
Date Acquired
August 10, 2013
Publication Date
September 1, 1979
Publication Information
Publication: NASA. Ames Res. Center Workshop on Thrust Augmenting Ejectors
Subject Category
Aerodynamics
Accession Number
80N10133
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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