It is assumed that flow is unidimensional; specific heats of gas are same before and after combustion; flow is adiabatic before combustion and that in sections of air inlet where there are no shock waves flow is isentropic; three main methods of measuring thrust; strain-gage method, thermodynamic method and aerodynamic method; charts giving results obtained in actual flight. In French with English translation of principal parts.
Flight measurements of ramjet and rocket thrust
Stato-reacteur ef fusee -- Determination de la poussee en vol
AGARD -- Reports ; n 196
1958
29 pages
Report
French
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Rocket Ramjet Boosters for Sustained High Speed Flight
British Library Conference Proceedings | 1997
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