M. Leroy Spearman

• A review of 50 years of aerodynamic research with NACA/NASA
• Aerodynamic characteristics of some lifting reentry concepts applicable to transatmospheric vehicle design studies
• Aerodynamics of a sphere and an oblate spheroid for Mach numbers from 0.6 to 10.5 including some effects of test conditions
• An experimental and theoretical study of the aerodynamic characteristics of some generic missles concepts at Mach numbers from 2 to 6.8
• An overview of some monoplanar missile programs
• Design trends for Army/Air Force airplanes in the United States
• Effects of body shape on the aerodynamics of a body of revolution at Mach numbers from 1.6 to 4.6
• Effects of external stores on the aerodynamic characteristics of a 60ê Delta-wing fighter model at Mach 1.60 to 2.87
• Effects of some geometric variations on missile aerodynamic characteristics at supersonic speeds
• Experimental and theoretical study of aerodynamic characteristics of some lifting bodies at angles of attack from -10 deg to 53 deg at Mach numbers from 2.30 to 4.62
• Experimental and theoretical study of aerodynamic characteristics of some lifting bodies at angles of attack from -10 to 53 at Mach numbers from 2.30 to 4.62
• Longitudinal aerodynamic characteristics at Mach numbers from 1.60 to 2.86 for a spanmissile with three wing planforms