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Effects of spanwise variation of leading-edge sweep on the lift, drag, and pitching moment of a wing-body combination at mach numbers 0. 7 to 2. 94(Effects of spanwise variation of leading edge sweep on lift, drag, & pitching moment of wing- body combination at transonic speeds)
Investigation of the Effects of Leading-edge Chord-extensions and Fences in Combination with Leading-edge Flaps on the Aerodynamic Characteristics at Mach Numbers from 0.40 to 0.93 of a 45 Degree Sweptback Wing of Aspect Ratio 4
Flight measurements of buffet characteristics of the F-104 airplane for selected wing-flap deflections(Flight tests to determine effects of moderate deflections of wing leading and trailing edges of F-104 aircraft buffet characteristics at subsonic and transonic speeds)
Influence of the trailing edge shape on the drag of a rectangular wing in the Mach number range from MA= 0. 5 to 2. 2(Influence of trailing edge thickness on aerodynamic drag of rectangular wings in transonic and supersonic flow)
Aerodynamic characteristics of three versions of a supersonic airplane model with a 45 deg sweptback midwing at Mach numbers of 1. 57 and 2. 01(Stability and drag studies for configurations of supersonic swept wing jet aircraft model at Mach numbers 1. 57 and 2. 01)
Improvement of maneuverability at high subsonic speeds(Fighter aircraft maneuverability improvement at high subsonic speeds by slotted and unslotted leading-and trailing-edge flaps on delta wing)