Axial and normal force coefficients for pointed bodies of revolution at super- and hypersonic speeds—Part II: Boattails

Regular price $23.00 $23.00 Sale

A study which serves as an aid to the aerodynamicist in optimizing missile design. Drag and lift increments are presented for a selected group of ogival and conical boattails (preceded by semi-infinite cylinders) in a Mach number range extending from...