NASA NTRS · 19800001894
The XFV-12A Thrust-Augmented Wing (TAW) prototype aircraft
Abstract
The 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.
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Murphy, R., Lewis, E. L.. 1979-09-01. The XFV-12A Thrust-Augmented Wing (TAW) prototype aircraft. https://ntrs.nasa.gov/citations/19800001894
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