Approximate solution of the problem of jet flow past an arc of a curve

1970 ◽  
Vol 22 (2) ◽  
pp. 200-203
Author(s):  
P. D. Karpenko
Keyword(s):  
Approximate Solution ◽  
Jet Flow ◽  
Flow Past

Jet Flow Past a Plate with a Spoiler in the Presence of a Stagnation Zone

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

Investigation of jet flow past slotted and wedge-shaped nozzles in a shock tube

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):  
Shock Tube ◽  
Jet Flow ◽  
Flow Past

General solution to the jet flow past a wedge

1984 ◽  
Vol 24 (3) ◽  
pp. 374-379
Author(s):  
V. I. Troshin
Keyword(s):  
General Solution ◽  
Jet Flow ◽  
Flow Past

Streamline jet flow past a thin profile bounded by a flow

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

Supersonic jet flow past an infinite wedge

1972 ◽  
Vol 4 (2) ◽  
pp. 70-71 ◽  
Author(s):  
E. G. Shifrin
Keyword(s):  
Supersonic Jet ◽  
Jet Flow ◽  
Flow Past ◽  
Infinite Wedge

Supercavitating Flow Past Slender Delta Wings

1959 ◽  
Vol 3 (04) ◽  
pp. 17-22
Author(s):  
Marshall P. Tulin
Keyword(s):  
Jet Flow ◽  
Cavitation Number ◽  
Conical Flow ◽  
Delta Wings ◽  
Flow Past ◽  
Supercavitating Flow ◽  
Leading Edges ◽  
Surface Increase

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.

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