Potential flow of segmental jet deflectors

Author:

Chang H. Y.,Conly J. F.

Abstract

A solution is developed for the deflexion of an inviscid, incompressible, twodimensional jet by a series of segments of arbitrary number, lengths, and angles. The Schwarz–Christoffel transformation and free-streamline theory are used. Results are calculated for a number of configurations, using an IBM 360 computer. Excellent comparison is found with several previous calculations for special cases.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference6 articles.

1. Tinney, E. R. , Barnes, W. E. , Rechard, O. W. & Ingram, G. R. 1961 Free-streamline theory for segmental jet deflectors.J. Hydraul. Div. Am. Soc. Civ. Engrs, HY5,135–145.

2. Siao, T. T. & Hubbard, P. G. 1953 Deflexion of jets, I, symmetrically placed V-shaped obstacle. Studies in Engineering , 35,State University of Iowa.

3. Copp, H. D. 1960 Laboratory investigations on trajectories from segmental flip buckets. M.S. Thesis,Washington State University.

4. Chang, H. Y. 1968 Flow analysis inside thrust reversers. Engineering Report 24–2287,Rohr Corp.,Chula Vista, California.

5. Bryan, G. H. & Jones, R. 1915 Discontinuous fluid motion past a bent plane, with special reference to aeroplane problems.Proc. Roy. Soc A91,354–70.

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