An innovative design feature of the Sonic Cruiser was its low drag inlets beneath the wings. Similar in cross section to the ovoid F-16 inlet but skewed outward, they stood proud from the airfame and clear of the boundary layer, ensuring a flow of "clean," undisturbed air into the shallow S-ducts feeding the buried engines. The configuration, revealed for the first time at the 2001 Paris Air Show, also posed some challenges, particularly with foreign-object ingestion.
To get around airline infrastructure concerns, Boeing presented airlines with alternative configurations. One was a "midwing" design that combined fairly conventional wings and tail surfaces with a "wasp-waisted" or area-ruled fuselage. The concept was configured with two main cabin cross sections, a wide cabin in the fore body and aft body, and a slimmer midbody section. The design resurrected a far reaching 1972 Boeing-NASA study that evaluated area-ruling in several concepts optimized for cruise speeds in the Mach 0.9 to .98 range.
Stargazer2006 said:Has anyone got an article (or a link) that would explain exactly why and how the Sonic Cruiser was canceled? This was the first transport program that I was really thrilled about and I never quite understood what killed it. All I know is that whenever "Sonic Cruiser" is pronounced, there always seem to be snide or derogatory remarks, if not outright laughs...
Sundog said:I too thought the Sonic Cruiser was the most exciting design going since the SST years, but it was too "radical" for the airline industry.
Sundog said:Boeing went back to the drawing board and came up with a maximum efficiency "safe" design, the 787. I say safe in the sense that people making the decisions think it looks the way an airplane is supposed to look. When, in fact, the 787 is probably more radical than the sonic cruiser was, due to it's structure and systems.
I've encountered this behavior in some of my engineering jobs, where I've designed something that looked quite different from what has been done before, but is actually quite safe from an engineering POV. Although, I did it to make the machines easier to manufacture, modify, and maintain. But then there is push-back from sales, "How are they going to sell that," and it isn't like what everyone else is doing. I thought the point was for us to NOT look like whatever one else is doing, to set us apart and be better; stupid f'n me.
Sundog said:the customer isn't always right and I've let them know that. I've been in trouble a few times for that, but it sure felt good letting them know it. ;D
LowObservable said:At the root of the problem was that the airplane was heavy. The wing was oversized because of the difficulty of installing effective flaps and because it needed a huge strake to carry fuel near the cg (the Starship problem). The engine installation threw away the bending-load relief of underwing engines (the VC10 problem). Then, to propel the aircraft in a high-drag zone, you needed more power (and more weight). I do not believe the design ever converged properly. As Norris points out, the aircraft needed a 90000 pound-class engine - a hell of a lot more than a 787 or A350 with similar or better payload and range.
LowObservable said:The Sonic Cruiser died because it made no sense in the first place. The total trip time savings for the passenger (from door to door) were attractive on very long sectors, but the price in terms of operating cost was very large.
Stargazer2006 said:Thanks for this interesting contribution, LowObservable!
Caravellarella said:I suspect "B" are still embarrassed by the whole episode......
Terry (Caravellarella)
Basil said:Does anyone know how the relative high bypass engine of the SC could have been operated economically at nearly Mach 1? It is my understanding that in these flight regimes the ideal bypass ratio should be much lower than that of a huge fan in front of the hot section.
Not to be beaten on the quiet airliner front, Boeing has refreshed its Sonic Cruiser design with a new patent (8,016,233, filed in 2006) that focuses on the canard double-delta configuration's ability to shield the noise from overwing-mounted engines.The patent also notes that the configuration's broad inboard wing section (and twin outboard vertical tails) could provide shielding of infrared radiation in a military application and shockwaves from the propulsion system in a supersonic configuration.
Skybolt said:Some correction/integration. Actually the sonic cruiser look-alike appeared on the cover of the NASA Office of Aeronautics Annual Report for 1999 "IS" a Boeing concept, more precisely configuration model 2154, one of the last developed during the HSCT program.
flateric said:Skybolt said:Some correction/integration. Actually the sonic cruiser look-alike appeared on the cover of the NASA Office of Aeronautics Annual Report for 1999 "IS" a Boeing concept, more precisely configuration model 2154, one of the last developed during the HSCT program.
Boeing Model 1080-2454 HiSCAT in 'sanitized' and 'de-sanitized' form.