Performance possibilities of the turbojet system as a power plant for supersonic airplanes

George P. Wood
Aug 1947

The performance of hypothetical turbojet systems, without thrust augmentation, as power plants for supersonic airplanes has been calculated. The thrust, thrust power, air-fuel ratio, specific fuel consumption, cross-sectional area, and thrust coefficient are shown for free-stream Mach numbers form 1.2 to 3.

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