General solution to the jet flow past a wedge

1984 ◽  
Vol 24 (3) ◽  
pp. 374-379
Author(s):  
V. I. Troshin
Keyword(s):  
Jet Flow ◽  
1992 ◽  
Vol 36 (01) ◽  
pp. 88-90
Author(s):  
David S. Tselnik

A number of plane inviscid jet flow problems of interest in hydrodynamics require the use of elliptic functions theory. Generally speaking, finding the general solution to a problem in terms of elliptic functions is not a complicated task. However, finding solutions as rapidly convergent infinite series or as sound asymptotic formulas is often not as easy, and special ways of treatment may prove to be necessary. In parallel with solving the problem of peripheral jets, the author's earlier paper (1985) proposed some such ways of treatment. In the present paper, a new method of treatment is proposed (and used);this approach may be of help in studies where the methods of elliptic functions theory have to be used.


2005 ◽  
Vol 40 (4) ◽  
pp. 532-539 ◽  
Author(s):  
D. V. Maklakov ◽  
G. M. Fridman
Keyword(s):  
Jet Flow ◽  

1983 ◽  
Vol 23 (6) ◽  
pp. 803-807
Author(s):  
V. V. Golub ◽  
V. V. Grigor'ev ◽  
Yu. I. Grin' ◽  
S. N. Isakov ◽  
I. M. Naboko ◽  
...  
Keyword(s):  
Jet Flow ◽  

1972 ◽  
Vol 7 (2) ◽  
pp. 308-310
Author(s):  
A. G. Terent'ev
Keyword(s):  
Jet Flow ◽  

1972 ◽  
Vol 4 (2) ◽  
pp. 70-71 ◽  
Author(s):  
E. G. Shifrin

1959 ◽  
Vol 3 (04) ◽  
pp. 17-22
Author(s):  
Marshall P. Tulin

The supercavitating flow past slender delta wings is studied. Theory is developed for a conical flow involving cavities which spring from the leading edges of the delta and cover a part of the top of the wing; the center part of the wing top is assumed to be wetted by a kind of re-entrant jet flow. Results are obtained for the two separate asymptotic cases in which the cavitation number is either very small or very large. The widths of the cavities on the wing upper surface increase with decreasing σ and the lift decreases. It is shown that the upper surface never becomes completely enveloped in a cavity even for σ = 0. Finally, the lift of a fully cavitated wing (σ = 0) is estimated to be approximately 4/10 of its fully wetted lift.


2014 ◽  
Vol 55 (2) ◽  
Author(s):  
Gioacchino Cafiero ◽  
Giuseppe Ceglia ◽  
Stefano Discetti ◽  
Andrea Ianiro ◽  
Tommaso Astarita ◽  
...  

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