S. Hoffman

发表

Free-flight investigation of the drag of a 60 deg delta-wing configuration with large stores mounted below the indented fuselage at mach numbers between 0.8 and 1.6

S. Hoffman, 1958 .

Summary of transformation equations and equations of motion used in free flight and wind tunnel data reduction and analysis

T. G. Gainer, S. Hoffman, T. Gainer, 1972 .