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Shockwave Images Help NASA In Development of 'Quiet' Supersonic Jet (go.com) 63

An anonymous reader writes: NASA is working on developing a next-generation supersonic jet that can break the sound barrier with a soft "thump" instead of a sonic boom. They are using a technique called schlieren imagery to "visualize supersonic flow phenomena with full-scale aircraft in flight" with the sun as the backdrop for the photos. According to a NASA blog post, viewing shock waves and their density is crucial to the project so engineers can work on a design to minimize those reverberations. While the Quiet Supersonic Technology (QueSST) research aircraft is being developed, stunning images were captured of a supersonic jet flying at Mach 1.05 with the sun in the background. NASA says when QueSST is operational, it could "unlock the future to commercial supersonic flight over land," essentially ushering in a new era of aviation that could allow us to get from point A to point B faster and without the loud roar of the Concorde as it breaks the sound barrier.
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Shockwave Images Help NASA In Development of 'Quiet' Supersonic Jet

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  • by Nutria ( 679911 ) on Thursday April 14, 2016 @10:53PM (#51913111)

    Are modern engines as efficient at Mach 1.5 as they are at Mach 0.9?

    • by Anonymous Coward on Thursday April 14, 2016 @11:07PM (#51913139)

      No, which is what doomed the Boeing Sonic Cruiser. Airlines prefer cheap operating costs over aircraft speed. In fact, they typically run their current fleet slower than the aircraft are able to cruise, for fuel economy reasons.

      • by NotAPK ( 4529127 )

        There's a bit more to the story than that.

        While Boeing was developing its own supersonic airliner, they were faced with the tough task of competing against Concorde, which was already established and flying. Instead of competing, the entrenched US aviation industry smeared the supersonic airline industry and encourage an FAA sanction prohibiting Concords (or any supersonic airliner) from flying supersonic over land.

        It's funny that they are now looking into this again, and all their old fear-mongering is bit

        • by XNormal ( 8617 )

          ... they were faced with the tough task of competing against Concorde, which was already established and flying ...

          ... and developed with French and British government funding. While the Concorde was operationally profitable for a while, it never made anywhere close to its original development costs. I can understand Boeing sour about it.

          • The reason the Concorde wasn't operational profitable was because it ws limited in routes. if it could fly, london, to newark, to la, to toyko, and then back to london it would have been better.

      • The Sonic Cruiser was never intended to go as fast as Mach 1.5, it was intended to hang around in the trans-sonic region (Mach 0.98 - 1.02 ish) and it was also intended to use the same engines as the Boeing 777 was using at the time. In the end, it was the fact that the aircraft was smaller than a 777, had much the same operating costs as the 777 and only arrived twenty or thirty minutes earlier than a 777 that killed it.

        Of course, Boeing received a lot of NASA funding for development into composite struct

      • No, which is what doomed the Boeing Sonic Cruiser. Airlines prefer cheap operating costs over aircraft speed. In fact, they typically run their current fleet slower than the aircraft are able to cruise, for fuel economy reasons.

        Many modern airliner engines have enough power to go supersonic. Obviously the airframes would make that not a good idea.

    • by AK Marc ( 707885 )
      The physics works differently at 0.9 than 1.1. For small planes, it may be easier to sustain 1.5, rather than 0.9. But the passenger jets aren't fighters, and would likely see increases for all increases in speed.
    • Are modern engines as efficient at Mach 1.5 as they are at Mach 0.9?

      You get to adjust the speed and pressure of the air in the engine - by a factor of several, if necessary - so the engine works well and makes good tradeoffs. That's much of what those cones, scoops, and funny-shaped housings are about, at least at the front. (Along the sides they're more about making room for the engine in the passing air without creating excessive drag.)

    • by Aviation Pete ( 252403 ) on Thursday April 14, 2016 @11:59PM (#51913255)

      Are modern engines as efficient at Mach 1.5 as they are at Mach 0.9?

      No. The engine doesn't notice the speed, the intake takes care of that. But to create thrust, the exhaust flow must be faster than the intake flow, and making the exhaust flow faster lowers the overall efficiency of the engine. This is why subsonic engines have a high bypass ratio while for supersonic engines bypass ratio must be kept low.

    • by AmiMoJo ( 196126 )

      The Japanese effort to developer supersonic passenger jets is looking to offset lower engine efficiency by reducing drag through aerodynamics and flying higher. Ideas include reconfigurable geometry and some advanced computer modelling that wasn't available when the last one was being designed in the 60s.

      It's still very experimental and may not work out, but maybe there is a way to overcome the issues.

    • by sycodon ( 149926 )

      Yes. [howstuffworks.com]

      The Raptor's two Pratt & Whitney F119-PW-100 engines pump out 35,000 pounds of thrust each (compare that to the 25,000-29,000 pounds of thrust for each engine on an F-15). Combined with the sleek aerodynamic design, the engines allow the Raptor to cruise at supersonic speeds with less fuel consumption than any other aircraft.

      So the technology is out there.

      • by Nutria ( 679911 )

        the engines allow the Raptor to cruise at supersonic speeds with less fuel consumption than any other aircraft.

        "Most efficient supersonic engines" != "More efficient than subsonic engines"

  • NASA or NACA? (Score:4, Interesting)

    by fsagx ( 1936954 ) on Thursday April 14, 2016 @11:02PM (#51913133)

    This headline could have been from the 40's or 50's. This is the way supersonic flow has been visualized as long as it has been studied. The supersonic wind tunnel and the Schlieren setup at the university I attended appeared pretty ancient to me in the 1980s.

    • by Anonymous Coward

      As mentioned in Wikipedia, Schlieren optics were developed to study supersonic motion in **1864**. Yes, 152 years ago. I'm happy to see it mentioned as it's a very simple but effective tool. When grinding my own Newtonian telescope mirror in 8th grade (1967) I noticed the Foucault knife test performed as a Schlieren system when a hand was placed near the mirror - the rising air currents from the warm hand are strikingly obvious.

      But headlining NASA's use of this is like headlining that Accountants use Arithm

    • by Sique ( 173459 )
      Most interesting is that the imaginery is still called schlieren optics. Schlieren is a german word meaning the streams and runmarks that can be seen if you mix two liquids of different optic properties like ink and water or Hydrogen peroxide and water.
      • by fsagx ( 1936954 )

        I remember my prof saying that it was German for "smear." I also remember thinking he was making that up, and assuming (wrongly, I find out 30 years later) it was really named for some guy named Schlieren. Thanks for the info!

  • by Anonymous Coward

    There aren't many people who complain that air travel isn't fast enough. The bigger issues are the hassles in airports and the cramped seating in planes, not that flights aren't fast enough. The real effect of this will be to increase carbon emissions, which is the last thing we need to be doing. After the past few years have been the hottest on record, we should be concerned with making travel more fuel-efficient instead of faster.

    • Being cramped in a plane for two hours instead of 10 sounds like an improvement to me.

      • Yeah, imagine if it was actually available. Normal flight, and express. Once you got used to flights five hours or less where ever you're going, it would be really hard going back to "slow" planes no matter how far back the business-seat reclines.

        If you never have to fly long distances, obviously you won't care. But if you do, particularly if you have to for business or family, paying up to save time becomes a real thing. In the day, business travelers loved the Concorde, 'cause they could fly to London

  • Why are they wasting tax dollars when the technology already has been known in Area 51 since the 1940s? The 1943 Wizarding
    Accords, of which the author of the Declaration of Independence, Labach the Elder, was a signatory, allowed such advanced technology to be exploited for civilian purposes. Smarten up, NASA!

  • NASA has to get a press release out about something. Can not have SpaceX making all the new science.

  • this makes great copy with images (which seems to be required thing for so called technology and science news stories regardless of substance ) but to design aircraft based on way they are photographed under particular conditions seems not to be the correct or safe way go about it.

  • by Aviation Pete ( 252403 ) on Thursday April 14, 2016 @11:56PM (#51913247)
    Supersonic flight adds a new source of drag, called wave drag [wikipedia.org], which comes on top of all other drag. It depends on the slenderness of the plane, but can easily double the total amount of drag. Optimizing the design for less pronounced shock waves will increase drag yet again, so fuel consumption per mile flown will make the cost of supersonic travel prohibitive. After all, the travel speeds of modern airliners (Mach 0.78 to 0.855) is typically a bit lower than the design speed of early jet airliners like the Convair 990 (Mach 0.87) or the Vickers VC-10 (Mach 0.89). That was half a century ago!

    But there is a pocket of aviation where progress has been made in flight speed: Business jets! While the first generation flew more slowly than airliners (Lockheed JetStar, Lear Jet 25), the latest designs are quite a bit faster (Cessna Citation X, Gulfstream V) at up to Mach 0.935. Why? There is a peeing contest going on among their owners who is the fastest. A very small segment of mankind is licking their fingers at a new chance for showing off. A supersonic business jet would be a sure sell to this crowd, even if the operating cost per mile doubles.

    Well, see it this way: This is a chance for the other 99.9% of mankind to lower the Gini coefficient [wikipedia.org] a bit.

    • by Maury Markowitz ( 452832 ) on Friday April 15, 2016 @06:21AM (#51914049) Homepage

      > Supersonic flight adds a new source of drag, called wave drag [wikipedia.org],

      As the author of the article you are linking to (if you don't believe me, click History and look) I find it somewhat odd that you apparently didn't *actually read it*.

      Wave drag is primarily and effect in the *transonic* from about M0.8 to 1.1 or 1.2, and then basically disappears at speeds above that. Jet airliners spend a significant portion of their flight time dealing with it, which is why it is important for modern air travel.

      Supersonic aircraft do indeed use much more fuel than subsonic, but it's not due (primarily) to wave drag, and designing to lower boom does not necessarily upset it for the worse.

      • Re: (Score:3, Interesting)

        Where does the article even hint at wave drag disappearing at higher supersonic speed?

        Wave drag is primarily and effect in the *transonic* from about M0.8 to 1.1 or 1.2, and then basically disappears at speeds above that.

        Wrong. Why don't you do some basic fact-checking yourself before wrongly accusing others?

        • by DRJlaw ( 946416 )

          Where does the article even hint at wave drag disappearing at higher supersonic speed?

          "The effect is typically seen on aircraft at transonic speeds (about Mach 0.8)..."

          I found it in less than 30 seconds.

          Wrong. Why don't you do some basic fact-checking yourself before wrongly accusing others?

          I'm certainly willing to completely trust conclusory statements simply thrown out there by "Aviation Pete." Especially ones that contradict the very source that such a self-professed fount of chose to cite in the first

  • "Where's the kaboom? There was supposed to be an earth shattering kaboom"
  • "technique called schlieren imagery"

    This is a terrible summary, and the linked articles aren't great either.

    This technique has been used since the 1800's, and specifically for supersonic aircraft design since the 1930s. If you poke about in Google Images you'll find German war-era photographs of swept-wing designs being tested. It was used for artillery design long before that.

    The real "news" here, which is hardly news because it's been used for a while now, is the use of outdoor photography to produce thes

  • Concorde "roar" was the takeoff power with reheat. The sonic boom is not a roar, it is a short bang [youtube.com]

    No-one near land heard Concorde's sonic boom. They all heard the engines, which were louder than a modern high-bypass turbofan.

  • by xxxJonBoyxxx ( 565205 ) on Friday April 15, 2016 @07:47AM (#51914321)
    >> allow us to get from point A to point B faster

    You really want to travel faster? Fire the TSA.
  • What is the point of making air travel faster when we have to spend hours in lines at the airport and getting to/from the airport? This only makes sense for really long trips like trans continent trips.

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