A computer program was developed to describe the performance of ramjet and scramjet cycles. The program performs one dimensional calculations of the equilibrium, real-gas internal flow properties of the engine. The program can be used for the following: (1) preliminary design calculation and (2) design analysis of internal flow properties corresponding to stipulated flow areas. Only the combustion of hydrogen in air is considered in this case.
Hypersonic ramjet experiment project. Phase 1: Computer program description, ramjet and scramjet cycle performance
14.06.1974
Report
Keine Angabe
Englisch
Springer Verlag | 2021
|NTIS | 1965
Pulsejet, Ramjet, and Scramjet Engines
Springer Verlag | 2016
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