Similarity in Vortex Asymmetries over Slender Bodies and Wings

Onset of aerodynamic side forces at zero sideslip on symmetric forebodies at high angles of attack

E. R. Keener, G. T. Chapman · Mechanics and Control of Flight Conference · 1974 · 110 citations

Engineering, Aerospace Engineering, Aerodynamics +16

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

E. R. Keener, G. T. Chapman, L. M. Cohen et al. · NASA Technical Reports Server (NASA) · 1977 · 68 citations

Engineering, Aerospace Engineering, Mechanical Engineering +17

Effects of Mach number and afterbody length on aerodynamic side forces at zero sideslip on symmetric bodies at high angles of attack

E. R. Keener, G. T. Chapman, Robert L. Kruse · 14th Aerospace Sciences Meeting · 1976 · 50 citations

Engineering, Aerospace Engineering, Mechanical Engineering +13

Side forces on forebodies at high angles of attack and Mach numbers from 0.1 to 0.7: two tangent ogives, paraboloid and cone

E. R. Keener, G. T. Chapman, J. Taleghani et al. · NASA STI Repository (National Aeronautics and Space Administration) · 48 citations · Full text

Engineering, Aerospace Engineering, Mechanical Engineering +17

Wind tunnel investigation of the aerodynamic characteristics of five forebody models at high angles of attack at Mach numbers from 0.25 to 2

E. R. Keener, J. Taleghani · NASA STI Repository (National Aeronautics and Space Administration) · 16 citations · Full text

Engineering, Aerospace Engineering, Mechanical Engineering +16