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A Simulation of a Supersonic Intake on a Hybrid Computer

Published online by Cambridge University Press:  07 June 2016

D.E. Colbourne
D.E. Colbourne*
Affiliation:
National Gas Turbine Establishment
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Summary

A simulation of the steady-state and dynamic performance of a supersonic powerplant intake is described. A lumped-parameter form of the equations of motion for a compressible fluid is developed. The resulting equations, together with steady-state characteristics, are used to model the performance of a two-dimensional supersonic intake. The model is implemented on the NGTE hybrid computer. The performance, both steady-state and transient, of the resulting real-time simulation has been investigated. Step and frequency responses at two high Mach number flight conditions have been examined and compared with test data. The favourable comparisons obtained demonstrate the validity of the chosen technique.

Type
Research Article
Information
Aeronautical Quarterly , Volume 31 , Issue 3 , August 1980 , pp. 197 - 220
Copyright
Copyright © Royal Aeronautical Society. 1980

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References

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