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.
The XFV-12A Thrust-Augmented Wing (TAW) prototype aircraft
1979-09-01
Miscellaneous
No indication
English
Thrust augmented wing sections in transition flight
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