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- Flutter of a 60©� delta wing (NACA 65A003 airfoil) encountered at supersonic speeds during the flight test of a rocket-propelled model
- Control hinge-movement and effectiveness characteristics of several interchangeable tip controls on a 60©� delta wing at Mach numbers of 1.41, 1.62, and 1.96
- On the range of applicability of the transonic area rule
- Supersonic flutter of a 60©� delta wing encountered during the flight test of a rocket-propelled model
- Investigation of the aerodynamic characteristics at high supersonic Mach numbers of a family of delta wings having double-wedge sections with the maximum thickness at 0.18 chord
- Wind-tunnel investigation at high subsonic speeds to determine the rolling derivatives of two wing-fuselage combinations having triangular winds, including a semiempirical method of estimating the rolling derivatives
- Effects of overhang balance on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing at transonic and supersonic speeds
- Effects of an inset tab on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60©� delta wing at Mach numbers from 0.75 to 1.96
- Wind-tunnel investigation of damping in roll at supersonic speeds of triangular wings at angles of attack
- Effects of two leading-edge modifications on the aerodynamic characteristics of a thin low-aspect-ratio delta wing at transonic speeds
- Low-speed static stability characteristics of a cambered-delta-wing model
- Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers
- Some measurements at subsonic speeds of the aerodynamic forces and moments on two delta wings of aspect ratios 2 and 4 oscillating about the midchord
- Effect at high subsonic speeds of fuselage forebody strakes on the static stability and vertical-tail-load characteristics of a complete model having a delta wing
- Aerodynamic characteristics of two delta wings and two trapezoidal wings at Mach number of 4.04