this post was submitted on 29 Sep 2026
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NASA is researching quieter supersonic flight, and I can't help but think of how the (also Lockheed Martin) X-59-
-has a extreme wing profile/nose, not unlike SR-71:
8700 lbs max doesn’t seem like a lot, are they counting on the parabola for most of the acceleration I wonder?
Its not very big. 8700 lb of fuel is 25% of its MGDW, which seems pretty normal to me?
I think the most likely explanation is something like this, they want data they can't otherwise get.
Machine learning + fluid dynamics?
Turbulence at the trans-sonic barrier is one of the most difficult and poorly understood problems in modeling even today - Heisenberg famously said he'd ask god two questions: why relativity, and why turbulence? - and as a result experimental results really are the best way of determining even the base parameters of the behavior of a system under those conditions.