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Effects of Two-Dimensional Inlet Configuration and Compression Surface Position on the Performance of Inlet Based on Ramjet Engine

Cao Jun-wei

Open publisher page 1 citations

Abstract

The calculation model of 2D hypersonic inlet is built,and the performance of supersonic inlet with three kinds of configurations and different compression surfaces position are investigated.The comparison results indicate that there are advantages and disadvantages to supersonic inlets with different configurations and compression surface positions.The conclusions are instructional to ascertain the project of supersonic inlet based on ramjet engine.

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What this paper is about

The calculation model of 2D hypersonic inlet is built,and the performance of supersonic inlet with three kinds of configurations and different compression surfaces position are investigated.The comparison results indicate that there are advantages and disadvantages to supersonic inlets with different configurations and compression surface positions.The conclusions are instructional to ascertain the project of supersonic inlet based on ramjet engine.

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Available abstract

The calculation model of 2D hypersonic inlet is built,and the performance of supersonic inlet with three kinds of configurations and different compression surfaces position are investigated.The comparison results indicate that there are advantages and disadvantages to supersonic inlets with different configurations and compression surface positions.The conclusions are instructional to ascertain the project of supersonic inlet based on ramjet engine.

Key concepts: Ramjet, Inlet, Supersonic speed, Aerospace engineering, Position (finance), Compression (physics), Turbofan, Hypersonic speed

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Effects of Two-Dimensional Inlet Configuration and Compression Surface Position on the Performance of Inlet Based on Ramjet Engine — Research Paper | ScholarLens