This survey presents a comprehensive investigation of blunt body dynamic stability. An examination of the experimental, analytical, and computational methods for predicting dynamic stability characteristics, along with the deficiencies accompanying each method is presented. The observed influence of vehicle and environmental parameters on the resulting dynamic response is discussed. Additionally, the proposed physical mechanisms that may govern this complex phenomenon are introduced. There exists a vast amount of literature and test data that is continually growing with each mission. Compiling the observations of dynamic behavior acquired from various test geometries, environments, and techniques, as well as the proposed explanations to the observed trends, sheds light on the validity of the proposed physical mechanisms. This in turn guides future efforts to improve the experimental and computational prediction techniques and further the fundamental understanding of blunt body dynamic stability.
NomenclatureA = Aerodynamic reference area, m 2 C D = Drag coefficient C L = Lift coefficient = Lift-curve slope = Pitching moment coefficient = Pitching moment slope = Pitch damping coefficient ̇ = Pitch damping sum CG = Center of gravity D = Reference diameter, m DOF = Degrees of freedom f = Oscillation frequency, Hz g = Acceleration due to gravity, m/s 2 h = Altitude, m I = Moment of inertia, kg-m 2 k = Reduced frequency parameter l = Characteristic length, m m = Mass, kg R = Radius from center of planet, m Sr, St = Strouhal number t = Time, s V = Velocity, m/s Greek α = Angle of attack, rad γ = Flight path angle, rad θ = Pitch angle, rad ξ = Dynamic stability parameter ρ = Atmospheric density, kg/m 3 ω = Angular velocity, rad/s Subscripts = Freestream condition