I understand that for a fighter aircraft, it would have to be inherently unstable. To do this I believe that the neutral point needs to be aft of the cg. I was told that during supersonic flight this relationship might be different. What would change in supersonic flight?

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    $\begingroup$ Would the answers to this question be of any help to answer this one? I feel we can mark your question as a duplicate - if you disagree, please edit your question and point out why it is not a dupe. $\endgroup$ Aug 12 '18 at 17:48
  • $\begingroup$ Yes I agree, thank you for the link appreciate it! $\endgroup$ Aug 13 '18 at 13:15