Accession Number:

AD0257616

Title:

RESEARCH ON RECIRCULATION WITHIN ROCKET COMBUSTION CHAMBERS

Descriptive Note:

Corporate Author:

SHEFFIELD UNIV (ENGLAND)

Personal Author(s):

Report Date:

1960-08-31

Pagination or Media Count:

1.0

Abstract:

The initial concept of a dynamically scaled model of an element of a real liquid fueled rocket combustion chamber incorporating phase change was developed. Photographic evidence of the recirculation patterns in this model were obtained. These patterns suggested that a live motor would have to be built to check the scaling laws and pattern similarity. Evidence from the cold model suggested some mechanisms for unstable combustion. Author

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE