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Of course they wont build it, that’s not the point. Unless you want to believe that Boeings CTO was talking out of his ass when offering specific details on what they can do with turboramjet tech, the simple truth is, Mach 5 is very possible.
Jack O’Banion, Vice President of Strategy and Customer Requirements, Advanced Development Programs for Lockheed Martin may have just unintentionally revealed that America’s next hypersonic warplane is much farther along the development process than previously suggested.
The purpose of O’Banion’s presentation of the SR-72 and its scramjet engine was to explain the critical role of digital advancements in designing and testing the aircraft and its engine in digital 3D models. He claims the digital transformation in recent years allowed the design to be robust with no moving parts, and to be extremely agile at hypersonic speeds.
Back in June, The War Zone reported that it was likely that the SR-72 was further along in development than initially presumed, and now it seems all but confirmed to be well clear of the conceptual and modeling phases of development, and possibly operational. The entire presentation seems to heavily suggest that Lockheed Martin either has completed an operational aircraft, or is incredibly close to achieving an operational aircraft.
originally posted by: anzha
That latter is the case, I'm pretty sure here and, hence, I think he's full of it.
originally posted by: TEOTWAWKIAIFF
Jan. 8, 2019 -
When hypersonic vehicle travels in the atmosphere with a high speed, the surrounding gas experiences complicated physical and chemical processes producing high-temperature gas effects. High-temperature gas effects are a key issue related to hypersonic aerodynamic design and optimization. The finite volume method is applied to solve unsteady three-dimensional compressible Navier–Stokes equations on unstructured meshes. High-temperature gas effects altering the aerodynamics of vehicle are taken into account. Possibilities of the use of graphics processor units (GPUs) for the simulation of hypersonic flows are demonstrated. Solutions of some benchmark test cases on GPUs are reported, and a comparison between computational results of chemically equilibrium reacting and perfect air flowfields is performed. Speedup of solution of the problems of interest on GPUs with respect to their solution on central processor units (CPUs) is compared. The results obtained provide promising perspective for designing a GPU-based software framework for applications in CFD.
originally posted by: MrSporkster
I think it's funny that the OP's alleged 'inside source' was wrong about Blackswift, which was cancelled in 2008.
originally posted by: MrSporkster
I think it's funny that the OP's alleged 'inside source' was wrong about Blackswift, which was cancelled in 2008.
originally posted by: Wgeorge666
a reply to: SpeedFanatic
Sacramento ca. Was on flight path of McClellan afb. No sound. Both times ive seen it was after midnight . no basis to know if manned or unmanned. But was amazing to see.
originally posted by: SpeedFanatic
a reply to: megamac
Hey megamac,
Great post, mate.
As for your sighting in the early 90's of a really loud aircraft that had 'triangle shape up front “connected” to a square shape in the rear.'.
You said it was late afternoon, so was it still daylight/sunset or so?
How would you describe size of the bird and what colour it had?
I suppose a location of the sighting was Cali?
Cheers!
A liquid injection scheme in a supersonic crossflow, namely transverse liquid injection accompanied with a gas jet, is proposed and investigated experimentally and numerically. High-speed photography was adopted to capture the jet spray in the experimental work; while a discrete phase model was utilized to simulate the liquid jet penetration and gas-liquid interaction in the numerical study. The differences between transverse liquid injection with and without an accompanied gas jet were analyzed. The effects of an accompanied gas jet were determined. Both the experimental and computational results indicate that an accompanied gas jet can significantly enhance liquid jet penetration. Simulation results also indicate that gas injection would cause additional total pressure losses.