Method and device for estimating the thrust of a ramjet

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738656, G01M 1500

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active

055896324

ABSTRACT:
The combustion chamber of the ramjet is mounted on a support which allows partial freedom of longitudinal movement. A nozzle is arranged at the intake of the combustion chamber, with a flexible, fluid-filled bladder being disposed between the nozzle and the combustion chamber. Air is blown into the combustion chamber through the nozzle, and fuel is fed into the combustion chamber to achieve combustion. The pressure of the fluid in the bladder is measured.

REFERENCES:
patent: 3038331 (1962-06-01), Henry et al.
patent: 3210991 (1965-10-01), Weekley
patent: 3537303 (1970-11-01), Hecht, Sr.
patent: 3788130 (1974-01-01), Ormond
patent: 4328703 (1982-05-01), McClure et al.
patent: 4788855 (1988-12-01), Laskody
patent: 5170662 (1992-12-01), Brault et al.
patent: 5235848 (1993-08-01), Hillenbrand
P. Rowe, "Laboratory Methods of Measuring Thrust," The Engineer, vol. 205, No. 5344, Jun. 27, 1958, pp. 964-967.

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