To paraphrase the Cuba Gooding character from “Jerry Maguire.”

I keep seeing these breathless articles in the popular media, and even the trade press, about reducing sonic boom, with its promise of practical commercial supersonic flight. The latest hype comes from Popular Science (via Clark Lindsey).

Why do I call them hype?

Two reasons.

First, I have never, ever seen a single number in these articles indicating to what degree the boom is attenuated. Maybe it’s just my suspicious nature, but I suspect that if we could see those numbers, we might be less impressed.

Second, there is never any mention in these articles about the other problem that is holding back practical supersonic flight, which is all of the drag associated with the shock. Even if by some legerdemain with vehicle contours they can reduce the boom sufficiently to allow overflight of land, the operating costs will remain horrific and unaffordable to most, because of the tremendous amount of wave drag from the shock system and skin drag from the huge swept delta wings that all of these concepts continue to employ.

That means that at best, it will remain another Concorde, though perhaps one that can fly coast to coast–an expensive ride only for the rich.

I find this topic particularly frustrating because I’ve been aware for a number of years of a technology with the potential to effectively eliminate shock, with both the sonic boom and the tremendous drag associated with it, but there has never been any interest in pursuing it, from either NASA or industry.

Anyway, I’ll take this stuff seriously when I see some quantification of just how much they’re reducing the overpressure, and some indication of understanding of the drag problem, instead of focusing entirely on the boom.

[Update in the afternoon]

Clark points out in comments that they do show some numbers in a slideshow.

Color me unimpressed. There’s never been any doubt that one can reduce boom through body shaping–the issue is whether you can get enough reduction to solve the problem. This graph shows a softer peak, from a little over 1.2 PSF to about 9 PSF. So they’re reducing it by about thirty percent.

Big whoop. Still gonna break windows.

Is there any reason to think that they can do significantly better than this graph would indicate, particularly for a large transport? There’s none provided in the article. In fact, they even admit in the caption here, “Designers of the modified F-5E weren’t trying to eliminate the sonic boom, but prove that aircraft shaping can lessen this signature of supersonic flight.”

Big deal–we knew that.

And as Clark notes, there remains no mention of the drag issue.

Still looks like hype to me, similar to that over hypersonics. It may be beneficial for some military apps, but there’s no reason to think that it will usher in a new era of commercial air transport, or even make supersonic bizjets practical, despite the pretty pictures.