Unsteady separated flows over three-dimensional slender bodies

Abstract Many review articles have been written on the topic of the aerodynamics of slender bodies at incidence, some of which are referenced in this paper. Here, we review the unsteady behavior of these flows. Our aim is to review the material that contributes to our understanding of unsteady phenomena over slender bodies at incidence. Natural unsteadiness is explored first. Unexpectedly, we found a large number of contributions in this area. We found the material disjointed, making it difficult to draw general conclusions. Forced unsteadiness is conceptually easier to follow, but the number of contributions on this topic is much smaller. We consider both experimental and numerical contributions but we do not discuss the corresponding methodologies.

[1]  David R. Williams,et al.  The effect of Reynolds number on control of forebody asymmetry by suction and bleed , 1993 .

[2]  Gerald N. Malcolm Forebody vortex control , 1991 .

[3]  Mv Lowson,et al.  Symmetry breaking in vortex flows on conical bodies , 1992 .

[4]  T. Yoshinaga,et al.  Coning motion of slender bodies at high angles of attack in low speed flow , 1981 .

[5]  Mikhail Goman,et al.  State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack , 1994 .

[6]  Chih-Ming Ho,et al.  Unsteady flow around an ogive cylinder , 1986 .

[7]  P. J. Lamont,et al.  AIAA 80-1556R Pressures Around an Inclined Ogive Cylinder with Laminar, Transitional, or Turbulent Separation , 2022 .

[8]  Louis Rosenhead,et al.  Laminar boundary layers , 1963 .

[9]  D. Telionis,et al.  Effect of coning motion and blowing on the asymmetric side forces on a slender forebody , 1997 .

[10]  K. Karamcheti,et al.  An experiment on the flow past a finite circular cylinder at high subcritical and supercritical Reynolds numbers , 1982, Journal of Fluid Mechanics.

[11]  L. B. Schiff,et al.  Aerodynamics of bodies of revolution in coning motion. , 1969 .

[12]  M. J. Stanek,et al.  Investigation of vortex development on a pitching slender body of revolution , 1991 .

[13]  Tetsushi Okamoto,et al.  The Experimental Investigation on the Flow Past a Circular Cylinder of Finite Length Placed Normal to the Plane Surface in a Uniform Stream , 1972 .

[14]  Matthew Zeiger,et al.  Vortex asymmetry over ogive cylinders in coning and pitching motions , 1996 .

[15]  D. Telionis Unsteady Viscous Flows , 1981 .

[16]  V. Theofilis Advances in global linear instability analysis of nonparallel and three-dimensional flows , 2003 .

[17]  Brent R. Cobleigh High-angle-of-attack yawing moment asymmetry of the X-31 aircraft from flight test , 1994 .

[18]  D. Degani,et al.  Numerical investigation of the origin of vortex asymmetry of flows over bodies at large angle of attack , 1990 .

[19]  P. Lamont The effect of Reynolds number on normal and side forces on ogive-cylinders at high incidence , 1985 .

[20]  Brian L. Hunt,et al.  Asymmetric vortex forces and wakes on slen-der bodies , 1982 .

[21]  B. L. Hunt,et al.  Pressure and force distributions on a sharp-nosed circular cylinder at large angles of inclination to a uniform subsonic stream , 1976, Journal of Fluid Mechanics.

[22]  The dynamic character of the vortical flow over a slender axisymmetric body , 2001 .

[23]  Patrick Reisenthel,et al.  The scaling and control of vortex geometry behind pitching cylinders , 1989 .

[24]  M. Bloor,et al.  The transition to turbulence in the wake of a circular cylinder , 1964, Journal of Fluid Mechanics.

[25]  L. Schiff,et al.  Results from a new wind-tunnel apparatus for studying coning and spinning motions of bodies of revolution , 1970 .

[26]  L. Ericsson Prediction of slender body coning characteristics , 1991 .

[27]  Lewis B. Schiff,et al.  NUMERICAL SIMULATION OF THE EFFECT OF SPATIAL DISTURBANCES ON VORTEX ASYMMETRY , 1989 .

[28]  Brian R. Kramer,et al.  F/A-18 and F-16 forebody vortex control, static and rotary-balance results , 1994 .

[29]  D. Degani,et al.  Numerical, experimental, and theoretical study of convective instability of flows over pointed bodies at incidence , 1991 .

[30]  G. T. Chapman,et al.  Side forces on a tangent ogive forebody with a fineness ratio of 3.5 at high angles of attack and Mach numbers from 0.1 to 0.7 , 1977 .

[31]  Demetri P. Telionis,et al.  Laminar separating flow over a prolate spheroid , 1987 .

[32]  Multi-sensor investigation of delta wing high-alpha aerodynamics , 1991 .

[33]  The dynamic character of the wake of an axisymmetric body at an angle of attack , 1991 .

[34]  David R. Williams,et al.  Proportional Control of Asymmetric Forebody Vortices , 1998 .

[35]  Steven E. Ramberg,et al.  The effects of yaw and finite length upon the vortex wakes of stationary and vibrating circular cylinders , 1983, Journal of Fluid Mechanics.

[36]  A. Wardlaw,et al.  Multistable vortex patterns on slender, circular bodies at high incidence , 1981 .

[37]  Morteza Gharib,et al.  An experimental study of the parallel and oblique vortex shedding from circular cylinders , 1991, Journal of Fluid Mechanics.

[38]  James Chen-yuan Wu,et al.  Unsteady viscous flow , 1975 .

[39]  David R. Williams,et al.  Closed-Loop Control of Forebody Flow Asymmetry , 1995 .

[40]  J. Gerrard,et al.  An experimental investigation of the end effects on the wake of a circular cylinder towed through water at low Reynolds numbers , 1981, Journal of Fluid Mechanics.

[41]  Patrick Reisenthel,et al.  Development of a nonlinear indicial model for maneuvering fighter aircraft , 1996 .

[42]  Cary Moskovitz,et al.  Effects of nose bluntness, roughness, and surface perturbations on the asymmetric flow past slender bodies at large angles of attack , 1989 .

[43]  D. Degani,et al.  Effect of splitter plate on unsteady flows around a body of revolution at incidence , 1991 .

[44]  C. Williamson Vortex Dynamics in the Cylinder Wake , 1996 .

[45]  J. P. Reding,et al.  Dynamics of Forebody Flow Separation and Associated Vortices , 1985 .

[46]  W. Calarese An Experimental Study of Vortex Flow on a Slender Body at Large Incidence , 1982 .

[47]  K. D. Thomson,et al.  The spacing, position and strength of vortices in the wake of slender cylindrical bodies at large incidence , 1971, Journal of Fluid Mechanics.

[48]  Charles H. K. Williamson,et al.  Vortex Dynamics in the Wake of a Cylinder , 1995 .

[49]  C. R. Smith,et al.  Secondary vortices in the wake of circular cylinders , 1986, Journal of Fluid Mechanics.

[50]  D. I. A. Poll,et al.  Some observations of the transition process on the windward face of a long yawed cylinder , 1985, Journal of Fluid Mechanics.

[51]  Robert M. Hall,et al.  Influence of Reynolds number on forebody side forces for 3.5-diameter tangent-ogive bodies , 1987 .

[52]  Roger L. Simpson,et al.  Unsteady measurements over a 6:1 prolate spheroid undergoing a pitch-up maneuver , 1994 .

[53]  L. E. Ericsson Unsteady flow separation on slender bodies at high angles of attack , 1993 .

[54]  Robert H. Nunn,et al.  Aerodynamic Characteristics of an Axisymmetric Body Undergoing a Uniform Pitching Motion , 1975 .

[55]  D. Degani,et al.  Asymmetric Vortices on a Slender Body of Revolution , 1991 .

[56]  J. P. Reding,et al.  Steady and Unsteady Vortex-Induced Asymmetric Loads on Slender Vehicles , 1981 .

[57]  D. A. Johnson,et al.  Control of forebody vortex orientation to alleviate side forces , 1980 .

[58]  D. Degani,et al.  Experimental study of nonsteady asymmetric flow around and ogive-cylinder at incidence , 1990 .

[59]  E. R. Keener,et al.  Flow-separation patterns on symmetric forebodies , 1986 .

[60]  Lewis B. Schiff,et al.  Forebody Tangential Slot Blowing on an Aircraft Geometry , 1994 .

[61]  P. Monkewitz,et al.  LOCAL AND GLOBAL INSTABILITIES IN SPATIALLY DEVELOPING FLOWS , 1990 .

[62]  David R. Williams,et al.  The effect of Reynolds number on vortex asymmetry about slender bodies , 1993 .

[63]  Roger L. Simpson,et al.  Unsteady Crossflow Separation Location Measurements on a Maneuvering 6:1 Prolate Spheroid , 1998 .