Alleviation of Vortex-Induced Asymmetric Loads

[1]  C. J. Apelt,et al.  The effects of wake splitter plates on bluff-body flow in the range 104 < R < 5 × 104. Part 2 , 1975, Journal of Fluid Mechanics.

[2]  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.

[3]  H. Julian Allen,et al.  Characteristics of flow over inclined bodies of revolution , 1951 .

[4]  G. T. Chapman,et al.  Onset of aerodynamic side forces at zero sideslip on symmetric forebodies at high angles of attack , 1974 .

[5]  A. H. Whitehead,et al.  Alleviation of vortex-induced heating to the lee side of slender wings in hypersonic flow , 1971 .

[6]  L. Ericsson,et al.  Maximum Vortex-Induced Side Force , 1978 .

[7]  E. R. Keener,et al.  Wind tunnel investigation of the aerodynamic characteristics of five forebody models at high angles of attack at Mach numbers from 0.25 to 2 , 1975 .

[8]  L. Ericsson,et al.  Maximum Side Forces and Associated Yawing Moments on Slender Bodies , 1979 .

[9]  Dhanvada M. Rao,et al.  Side-Force Alleviation on Slender, Pointed Forebodies at High Angles of Attack , 1979 .

[10]  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 .

[11]  L. Ericsson.  Aeroelastic instability caused by slender payloads. , 1967 .

[12]  J. R. Chambers,et al.  Asymmetric lateral-directional characteristics of pointed bodies of revolution at high angles of attack , 1972 .

[14]  J. P. Reding,et al.  Maximum side forces and associated yawing moments on slender bodies , 1979 .

[15]  C. Mcelroy,et al.  An approach to stall/spin development and test , 1971 .

[16]  Edward W Perkins,et al.  A study of the effects of body shape on the vortex wakes of inclined bodies at a Mach number of 2 , 1953 .

[17]  G. T. Chapman,et al.  Effects of Mach number and afterbody length on aerodynamic side forces at zero sideslip on symmetric bodies at high angles of attack , 1976 .

[18]  R. C. Nelson,et al.  High Angle-of-Attack Aerodynamics on a Slender Body with a Jet Plume , 1975 .