Publication Date:
2016-06-07
Description:
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.
Keywords:
AERODYNAMICS
Type:
NASA. Ames Res. Center Workshop on Thrust Augmenting Ejectors; p 473-480
Format:
application/pdf