Browse TRAIL Inventories

Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles

Aerodynamic characteristics of a delta wing with leading edge swept back 45 degrees, aspect ratio 4, and NACA 65A006 airfoil section.Transonic-bump method

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

Effects of two leading-edge modifications on the aerodynamic characteristics of a thin low-aspect-ratio delta wing at transonic speeds

Wind-tunnel investigation of damping in roll at supersonic speeds of triangular wings at angles of attack

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


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