An investigation of both an experimental and theoretical nature has been conducted into the use of a subsonic conventional ejector as a thrust augmentor. A new effectiveness performance parameter, EN, was derived in this investigation and has proved a useful tool in comparing different thrust augmentor designs. Moderate ejector diffuser area ratios, around 1.5:1, were round to he more favourable for thrust augmentation. This dis(')very proves a new concept in ejector augmentor design which is more suitablc in airfield applications.
EL-BANNA, R. (1987). NEW CONCEPTS IN THRUST AUGMENTOR EJECTORS. International Conference on Aerospace Sciences and Aviation Technology, 2(A.S.A.T. CONFERENCE 21-23 April 1987 , CAIRO), 311-323. doi: 10.21608/asat.1987.26006
MLA
RAMADAN AHMED EL-BANNA. "NEW CONCEPTS IN THRUST AUGMENTOR EJECTORS", International Conference on Aerospace Sciences and Aviation Technology, 2, A.S.A.T. CONFERENCE 21-23 April 1987 , CAIRO, 1987, 311-323. doi: 10.21608/asat.1987.26006
HARVARD
EL-BANNA, R. (1987). 'NEW CONCEPTS IN THRUST AUGMENTOR EJECTORS', International Conference on Aerospace Sciences and Aviation Technology, 2(A.S.A.T. CONFERENCE 21-23 April 1987 , CAIRO), pp. 311-323. doi: 10.21608/asat.1987.26006
VANCOUVER
EL-BANNA, R. NEW CONCEPTS IN THRUST AUGMENTOR EJECTORS. International Conference on Aerospace Sciences and Aviation Technology, 1987; 2(A.S.A.T. CONFERENCE 21-23 April 1987 , CAIRO): 311-323. doi: 10.21608/asat.1987.26006
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