Browse TRAIL Inventories

Aerodynamic characteristics of a wing with quarter-chord line swept back 35©�, aspect ratio 6, taper ratio 0.6, and NACA 65A006 airfoil section.Transonic-bump method

Results of two free-fall experiments on flutter of thin unswept wings in the transonic speed range

An investigation at transonic speeds of the effects of thickness ratio and of thickened root sections on the aerodynamic characteristics of wings with 47©� sweepback, aspect ratio 3.5, and taper ratio 0.2 in the slotted test section of the Langley 8-foot high-speed tunnel

Error in airspeed measurement due to static-pressure field ahead of an open-nose air-inlet model at transonic speeds

Miscellaneous directional-stability data for several airplane-like configurations from rocket-model tests at transonic speeds

Effect of longitudinal wings position on the pressure characteristics at transonic speeds of a 45©� sweptback wing-fuselage model

On the range of applicability of the transonic area rule

Effects of fences, leading-edge chord-extensions, bound-layer ramps, and trailing-edge flaps on the longitudinal stability of a twisted and cambered 60©� sweptback-wing--indented-body configuration at transonic speeds

The effects of wing incidence on the aerodynamic loading characteristics of a sweptback wing-body combination at transonic speeds

An experimental transonic investigation of a 45©� sweptback wing-body combination with several types of body indentation with theoretical comparisons included

On slender-body theory at transonic speeds

An investigation of the effects of a geometric twist on the aerodynamic loading characteristics of a 45©� sweptback wing-body configuration at transonic speeds

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

Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a diamond-plan-form wing aspect ration 3.08 and a low, swept horizontal tail

Characteristics of loads in rough air at transonic speeds of rocket-powered models of a canard and a conventional-tail configuration

An experimental study of a method of designing the sweptback-wing - fuselage juncture for reducing the drag at transonic speeds

Loads on thin wings at transonic speeds

Investigation at transonic speeds of the hinge-moment characteristics of a 1/8-scale model of the X-1E aileron

Transonic wind-tunnel investigation of the effects of sweepback and thickness ratio on the wing loads of a wing-body combination of aspect ratio 4 and taper ratio 0.6

Effect of a reduction in stator solidity on performance of a transonic turbine

Transonic investigation at lifting conditions of streamline contouring in the sweptback-wing-fuselage juncture in combination with the transonic area rule

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

Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches

Investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections

Steady loads due to jet interference on wings, tails, and fuselages at transonic speeds

Investigation of transonic flutter characteristics of a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6

Span loadings due to wing twist at transonic and supersonic speeds

Investigation of fixed-geometry supersonic inlets with bypass ducts for matching turbojet-engine air-flow requirements over a range of transonic and supersonic speeds


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