The problem of the slosh of an inviscid lf.quid partially filling a rigiogulindrical tank is studied theoretically. The tank is connected - through an outlet at its base - with a pump that causes a velocity fluctuation at the outlet due to its pressure. The nonlinear' governing equations have been constructed and their solution accompanied by the stability is given. It has been found that the results reduce to the results of previous investigations in proper limits.
SAFWAT, H. (1987). LIQUID SLOSH DUE TO A PULSATING SOURCE. International Conference on Aerospace Sciences and Aviation Technology, 2(A.S.A.T. CONFERENCE 21-23 April 1987 , CAIRO), 393-406. doi: 10.21608/asat.1987.26179
MLA
HELMY MUHAMMAD SAFWAT. "LIQUID SLOSH DUE TO A PULSATING SOURCE". International Conference on Aerospace Sciences and Aviation Technology, 2, A.S.A.T. CONFERENCE 21-23 April 1987 , CAIRO, 1987, 393-406. doi: 10.21608/asat.1987.26179
HARVARD
SAFWAT, H. (1987). 'LIQUID SLOSH DUE TO A PULSATING SOURCE', International Conference on Aerospace Sciences and Aviation Technology, 2(A.S.A.T. CONFERENCE 21-23 April 1987 , CAIRO), pp. 393-406. doi: 10.21608/asat.1987.26179
VANCOUVER
SAFWAT, H. LIQUID SLOSH DUE TO A PULSATING SOURCE. International Conference on Aerospace Sciences and Aviation Technology, 1987; 2(A.S.A.T. CONFERENCE 21-23 April 1987 , CAIRO): 393-406. doi: 10.21608/asat.1987.26179
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