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Investigation of aerodynamic characteristics at high subsonic speeds of two supersonic- cruise airplane configurations having tail surfaces outboard of the wing tips
Subsonic stability and control characteristics of two outboard-tail supersonic-cruise airplane configurations
Analytical study of effects of product of inertia on airplane spin entries, developed spins, and spin recoveries
Inertia product and inertia moment variation effect on spin entry, developed spin, and spin recovery of airplanes
Flow field survey and decelerator drag characteristics in the wake of a model of the X-15 airplane at Mach 2.30 and 4.65
Flow field survey and decelerator drag characteristics in wake of model X-15 airplane at Mach 2.30 and 4.65
Flight investigation of steep instrument approach capabilities of a T-33 airplane under manual control
Steep instrument approach capabilities of T-33 airplane under manual control from glide slope to touchdown
Effects of Boattail Area Contouring and Simulated Turbojet Exhaust on the Loading and Fuselage-tail Component Drag of a Twin-engine Fighter-type Airplane Model
Effects of boattail area contouring and simulated turbojet exhaust on loading and fuselage-tail component drag of twin-engine fighter-type airplane model
Flutter studies of simplified component models of a variable-sweep-wing airplane at Mach numbers up to 3.0
Wind tunnel flutter analysis of simplified component models of variable-sweep-wing airplane at Mach numbers up to 3
Transonic Flutter Investigation of Models of the Sweptback Wing of a Fighter Airplane
Transonic flutter characteristics of sweptback fighter airplane wing models
Analysis of Flight-determined and Predicted Effects of Flexibility on the Steady-state Wing Loads of the B-52 Airplane
Flight-determined and predicted effects of flexibility on steady-state wing loads of B-52 airplane
The influence of airplane configuration on the shape and magnitude of sonic-boom pressure signatures.
Airplane configuration effect on shape and magnitude of sonic boom pressure signature, noting theoretical and empirical methods
Noise measurement evaluations of various takeoff-climbout profiles of a four-engine turbojet transport airplane
Noise measurement evaluations of various takeoff-climbout profiles of four engine turbojet transport airplane
Statistical analysis of landing contact conditions of the X-15 airplane
Statistical analysis of landing contact conditions and slideout distances of X-15 research airplane
An analysis of VGH data from one type of four-engine turbojet transport airplane during commercial operations
Velocity, gust, and height data analysis from four-engine turbojet transport airplane
Subsonic and transonic flutter and flow investigations of the T-tail of a large multijet cargo airplane
Subsonic and transonic flutter and flow studies of T tail of large multijet cargo airplane
Effects of simulated wing damage on the aerodynamic characteristics of a swept-wing airplane model
Simulated wing damage effects on aerodynamic characteristics of swept-wing airplane model
Summary of VGH data collected on one type of twin-engine jet airplane during airline operations
Summary of vertical gusts acceleration data collected for one type twin engine jet airplane during airline operations
Analysis of airplane design by similarity considerations.
Airplane design analysis by operational similarity parameters and coefficients, noting aircraft applications range from DC-3 to SST
Wind-tunnel study of deflected-elevator flutter encountered on a T-tail airplane
Wind tunnel study of deflected elevator flutter encountered on T-tail airplane