A Discussion of Two-Dimensional Turbulent Base Flows By

The paper presents a review of recent experimental and theoretical research on two-dimensional base flows. The main object is to illustrate the extent to which the basic properties of the flow are understood in each of the different flow r6gimes : subsonic periodic, subsonic non-periodic, and supersonic. The main conclusion from this study is that further work is needed throughout the whole field, but attention is drawn to those areas where the need is most urgent.

[1]  A. Mager.  Transformation of the Compressible Turbulent Boundary Layer , 1958 .

[2]  P. Libby.  The Scientific American , 1881, Nature.

[3]  Luigi Crocco,et al.  A Mixing Theory for the Interaction between Dissipative Flows and Nearly-Isentropic Streams , 1952 .

[4]  A study of the turbulent separated-flow region occurring at a compression corner in supersonic flow , 1965 .

[5]  C. Wood,et al.  The Effect of Base Bleed on a Periodic Wake , 1964, Journal of the Royal Aeronautical Society.

[6]  Dean R. Chapman,et al.  Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition , 1958 .

[7]  P. G. Hill,et al.  Turbulent Wakes in Pressure Gradients , 1963 .

[8]  Dean R Chapman,et al.  An analysis of base pressure at supersonic velocities and comparison with experiment , 1951 .

[9]  R. J. Stalker.  Sweepback Effects in Turbulent Boundary-Layer Shock-Wave Interaction , 1960 .

[10]  The development of turbulent boundary layers with negligible wall stress , 1960 .

[11]  A. F. Charwat,et al.  An Investigation of Separated Flows - Part I: The Pressure Field , 1961 .

[12]  Lester Lees,et al.  SUPERSONIC SEPARATED AND REATTACHING LAMINAR FLOWS: I. GENERAL THEORY AND APPLICATION TO ADIABATIC BOUNDARY LAYER-SHOCK WAVE INTERACTIONS. , 1964 .

[13]  M. Badrinarayanan.  An Experimental Investigation of Base Flows at Supersonic Speeds , 1961, The Journal of the Royal Aeronautical Society.

[14]  J. Gerrard,et al.  An experimental investigation of the oscillating lift and drag of a circular cylinder shedding turbulent vortices , 1961, Journal of Fluid Mechanics.

[15]  G. Kleinstein,et al.  Mixing in turbulent axially symmetric free jets , 1964 .

[16]  B. Stratford.  The prediction of separation of the turbulent boundary layer , 1959, Journal of Fluid Mechanics.

[17]  Jacob E. Fromm,et al.  Computer Experiments in Fluid Dynamics , 1965 .

[18]  Peter W. Bearman,et al.  Investigation of the flow behind a two-dimensional model with a blunt trailing edge and fitted with splitter plates , 1965, Journal of Fluid Mechanics.

[19]  Theory for Supersonic, Two-Dimensional, Laminar, Base-Type Flows Using the Crocco-Lees Mixing Concepts , 1962 .

[20]  L. H. Townend,et al.  Some effects of stable combustion in wakes formed in a supersonic stream , 1963 .

[21]  H. Mcdonald.  An Analysis of the Turbulent Base Pressure Problem in Supersonic Axisymmetric Flow , 1965 .

[22]  A. Roshko.  On the Wake and Drag of Bluff Bodies , 1955 .

[23]  H. Mcdonald.  The Turbulent Supersonic Base Pressure Problem: A Comparison between a Theory and Some Experimental Evidence , 1966 .

[24]  Maurice Tucker,et al.  Effect of a Discontinuity on Turbulent Boundary-Layer-Thickness Parameters With Application to Shock-Induced Separation , 1955 .

[25]  J. Rom.  Analysis of the near-wake pressure in supersonic flow using the momentum integral method. , 1966 .

[26]  Jack N. Nielsen,et al.  CALCULATION OF LAMINAR SEPARATION WITH FREE INTERACTION BY THE METHOD OF INTEGRAL RELATIONS. PART 1. TWO-DIMENSIONAL SUPERSONIC ADIABATIC FLOW , 1965 .

[27]  A. Roshko,et al.  Observations of turbulent reattachment behind an axisymmetric downstream-facing step in supersonic flow. , 1966 .