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- 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
- 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 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
- 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
- An experimental study of a method of designing the sweptback-wing - fuselage juncture for reducing the drag at transonic speeds
- Characteristics of loads in rough air at transonic speeds of rocket-powered models of a canard and a conventional-tail configuration
- 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
- 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
- Steady loads due to jet interference on wings, tails, and fuselages at transonic 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