gambit
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Essentially -- yes.Still can't supercruise,but yes as low observable strike aircraft why not. @gambit
How does thrust work for 2 engines?Just addition of 2 thrusts?I doubt it.
Patent US5480107 - 3x multi-engine jet configuration - Google Patents
But there are many factors that affect the attainment of a desired speed.2x Conventional Jet. This represents modeled data based upon a popular entry level business jet in current use, and generally depicted in FIG. 6. The 2x conventional Jet uses twin WILLIAMS/ROLLS ROYCE-manufactured engines (32 and 34 with reference to FIG. 6) of 1,900 pounds thrust each. The engines are mounted on the left and right rear of the fuselage and will be referred to as 1x (left) and 1x (right). The 2x conventional jet will develop a total (2x) thrust of 3,800 pounds.
Two aircrafts comes to mind: SR-71 and F-104. Both have shapes that are optimized for acceleration (which is not the same as speed), speed, then the sustainment of said speed.
For multi-engine aircrafts, asymmetric thrust affects acceleration, speed, and sustainment of achieved speed. This is simple for the fact that the aircraft should present the least drag profile to the airstream. Asymmetric thrust, especially for the SR-71 with its wide engine spacing, will probably prevent Mach, let alone sustain it. The F-104 would not have this potential problem.
Another factor is drag from the engine itself. A ramjet have no moving parts and therefore the least drag loss to affect net thrust. On the other hand, a turbo-whatever have plenty of moving parts, especially the fan stages that must be exposed to incoming airstream in order to have air to create the air-fuel mixture and burn it.
Then add in airframe design which give aerodynamics, and weight and we have plenty of variables that can prevent an aircraft from attaining supercruise despite being multi-engine.
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