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Separated Flow about Cones at Incidence—Theory and Experiment

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Studies of Vortex Dominated Flows

Part of the book series: ICASE NASA LaRC Series ((ICASE/NASA))

Abstract

The motivation for the work described here is the study, understanding and ultimate prediction of separated flow past bodies at incidence. The work has concentrated on modelling, mathematically, the vortical flow about slender bodies at incidences where the separation starts at the pointed apex of the body. Separation can, of course, occur further back along the body, particularly if the body is quite long, ie of high fineness ratio. However, a major interest of the work has been in understanding the development of lateral asymmetry in the flow about laterally symmetric bodies at moderate to high incidences, for cases where the separation has moved forward to the apex for typical bodies, eg an ogive-cylinder combination. The importance of the nose region in determining the development of separation asymmetry is emphasized by the fact that many of the ‘fixes’ proposed to reduce the degree of flm’l asymmetry involve modifying the nose, eg nose blunting, strakes, blowing at the apex, adding small pieces of grit very near the nose tip, etc.

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References

  1. W.J. Rainbird. “The external flow field about yawed circular cones.” Paper 19 in AGARD CP-30 (1968)

    Google Scholar 

  2. D.J. Peake, F.K. Owen, D.A. Johnson. “Control of fore body vortex orientation to alleviate side-forces.” AIAA Paper 80-0183 (1980)

    Google Scholar 

  3. A.E. Bryson. “Symmetrical vortex formation on circular cylinders and cones.” J. Appl. Mech. (ASME) 26., 643–8 (1959)

    MathSciNet  MATH  Google Scholar 

  4. D.E. Dyer, S.P. Fiddes, J.H.B. Smith. “Asymmetric vortex formation from cones at incidence - a simple inviscid model.” Aeronautical Quarter, 33 293–312 (1982)

    Google Scholar 

  5. S.P. Fiddes. “A theory of the separated flow past a slender elliptic cone at incidence.” Paper 30 in AGARD CP-291 (1980)

    Google Scholar 

  6. R. Legendre. Ecoulement au voisinage de la pointe avant d’une aile a forte fleche aux incidences moyennes.8th Int. Congr. Th. Appl. Mech., Istanbul (1952)

    Google Scholar 

  7. K.P. Mangler, J.H.B. Smith. “A theory of the separated flow past a slender delta wing with leading-edge separation.” Proc. Roy. Soc. London A, 251, 200–217 (1959)

    Article  MathSciNet  ADS  MATH  Google Scholar 

  8. J.H.B. Smith. “Improved calculations of leading-edge separation from slender, thin delta wings.” Proc. Roy, Soc. London A, 306, 67–90 (1968)

    Article  ADS  MATH  Google Scholar 

  9. J.H.B. Smith. “Behpviour of a vortex sheet separating from a smooth surface.” RAE Technical Report 77058 (1978)

    Google Scholar 

  10. F.T. Smtth. “Three-dimensional viscous and inviscid separation of a vortex sheet from a smooth non-s lender body.” RAE Technical Report 78095 (1979)

    Google Scholar 

  11. S.P. Fiddes, J.H.B. Smith. “Calculations of asymmetric separated flow past circular cones at large angles of incidence.” Paper 14 in AGARD CP-336 (1982)

    Google Scholar 

  12. D.N. Decker, H.B. Keller. “Path following near bifurcation.” Corom. Pure App1. Math. 34149–175 (1981)

    Article  MathSciNet  MATH  Google Scholar 

  13. A.R.G. Mundell. RAE unpublished (1982).

    Google Scholar 

  14. J.S. Smith. “Preliminary tests of slender bodies in the 5m pressurised low-speed tunnel.” RAE Technical Memorandum Aero 1973 (1983)

    Google Scholar 

  15. I.R.M. Moir. “Recent experience in the RAE 5m wind tunnel of a china-clay technique for indicating boundary-layer transition.” RAE Technical Memorandum Aero 2007 (1984)

    Google Scholar 

  16. E.R. Keener, G.T. Chapman, L. Cohen, J. Taleghani. Side forces on a tangent ogive fore body with a fineness ratio of 3.5 at high angles of attack and Mach numbers from 0.1 to 0.7.” NASA TM X-3437 (1977)

    Google Scholar 

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© 1987 Springer-Verlag New York Inc.

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Fiddes, S.P. (1987). Separated Flow about Cones at Incidence—Theory and Experiment. In: Hussaini, M.Y., Salas, M.D. (eds) Studies of Vortex Dominated Flows. ICASE NASA LaRC Series. Springer, New York, NY. https://doi.org/10.1007/978-1-4612-4678-7_13

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  • DOI: https://doi.org/10.1007/978-1-4612-4678-7_13

  • Publisher Name: Springer, New York, NY

  • Print ISBN: 978-0-387-96430-0

  • Online ISBN: 978-1-4612-4678-7

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