Publication Date:
2019-06-27
Description:
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.
Keywords:
PROPULSION SYSTEMS
Type:
NASA-CR-132454
,
AP-1001-1
Format:
application/pdf