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Oh the subject of the difficulties that GD had with twin vertical stabilizers in their ATF proposal, the F-22 would also end up encountering problems with vibrations and buffeting in the vertical tails at certain Mach numbers and g conditions, due to the vortex impingement at those specific conditions. This was reported back in 2000.


[URL unfurl="true"]https://www.flightglobal.com/buffeting-problem-may-mean-airframe-changes-for-f-22-/34405.article[/URL]


According to Jay Miller’s book on the F-22, this issue was eventually resolved with some strengthening of the vertical tails and flight control software changes.


Still, this makes me a bit curious on why GD abandoned twin canted vertical stabilizers. Perhaps there wasn’t enough time for them to fine-tune a satisfactory configuration before the RFP submission? Along with the inlet, vertical tails took among the longest time in wind tunnel testing for the Lockheed/Boeing/General Dynamics team, and even then, there ended up being buffeting from flow impingement that modeling had failed to predict.


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