Aerodynamic Characteristics of a Family of Cone-Cylinder-Flare Projectiles
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[1] C. H. Murphy. DATA REDUCTION FOR THE FREE FLIGHT SPARK RANGES , 1954 .
[2] Clarence A. Syvertson,et al. A Second-Order Shock-Expansion Method Applicable to Bodies of Revolution Near Zero Lift , 1957 .
[3] R. V. Owens. Aerodynamic characteristics of spherically blunted cones at Mach numbers from 0.5 to 5.0 , 1965 .
[4] T. J. Mueller,et al. Influence of initial flow direction on the turbulent base pressure in supersonic axisymmetric flow , 1970 .
[5] H. Lomax,et al. Thin-layer approximation and algebraic model for separated turbulent flows , 1978 .
[6] R. F. Warming,et al. An Implicit Factored Scheme for the Compressible Navier-Stokes Equations , 1977 .
[7] Lewis B. Schiff,et al. Numerical Simulation of Steady Supersonic Viscous Flow , 1979 .
[8] S. Vukelich,et al. Missile DATCOM - Aerodynamic prediction of conventional missiles using component build-up techniques , 1984 .
[9] I. Celmins. Drag and stability tradeoffs for flare-stabilized projectiles , 1990 .