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- Effect of spanwise variations in gust intensity on the lift due to atmospheric turbulence
- A collection of data for zero-lift damping in roll of wing-body combinations as determined with rocket-powered models equipped with roll-torque nozzles
- Effects of conical camber on the lift, drag, and pitching-moment characteristics of a triangular wing of aspect ratio 3.0
- Effects of extreme surface cooling on boundary-layer transition
- A comparison of typical National Gas Turbine Establishment and NACA axial-flow compressor blade sections in cascade at low speed
- Effect of interstage bleed on rotating stall and blade vibration in a 13-stage axial-flow compressor in a turbojet engine
- The design and cascade tests of free-streamline and full-contour 160 degrees turning supersonic-turbine-blade sections
- Design and experimental investigation of a single-stage turbine with a downstream stator
- Design and test of mixed-flow impellers 8: comparison of experimental results for three impellers with shroud redesigned by rapid approximate method
- The interrelated effects of engine rotor momentum and flight regime on the dynamic stability of high-performance aircraft
- Effects of vertical location of wing and horizontal tail on the aerodynamic characteristics in pitch at Mach numbers from 0.60 to 1.40 of an airplane configuration with an unswept wing
- Effects of wing-mounted external stores on the longitudinal and lateral handing qualities of the Douglas D-558-II research airplane
- Effects of wing warp on the lift, drag, and static longitudinal stability characteristics of an aircraft configuration having an arrow wing of aspect ratio 1.86 at Mach numbers from 1.1 to 1.7
- Analysis of shock motion in ducts during disturbances in downstream pressure
- A hydrogen peroxide turbojet-engine simulator for wing-tunnel powered-model investigations
- Experimental investigation of dynamic relations in a 48-inch ram-jet engine
- The application of matrix methods to coordinate transformations occurring in systems studies involving large motions of aircraft
- An analog computer study of several stability augmentation schemes designed to alleviate roll-induced instability
- Application of obliquely mounted strain gage to measurement of residual stresses in disks
- A balanced-pressure sliding seal used for transfer of pressurized air between stationary and rotating parts
- Base pressure at supersonic speeds on two-dimensional airfoils and on bodies of revolution with and without fins having turbulent boundary layers
- Investigation of semivaneless turbine stator designed to produce axially symmetrical free-vortex flow
- Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study 2: design and experimental performance of turbine with low-velocity-turning stator and standard rotor
- Jet effects on base pressures of conical afterbodies at Mach 1.91 and 3.12
- Static longitudinal and lateral stability characteristics at low speed of 45 degree sweptback-midwing models having wings with an aspect ratio of 2, 4, or 6
- Wind-tunnel investigation of external-flow jet-augmented double slotted flaps on a rectangular wing at an angle of attack of 0 degree to high momentum coefficients
- Wind-tunnel investigation of effect of propeller slipstreams on aerodynamic characteristics of a wing equipped with a 50-percent-chord sliding flap and a 30-percent-chord slotted flap
- Wind-tunnel investigation of effects of ground proximity and of split flaps on the lateral stability derivatives of a 60 degree delta-wing model oscillating in yaw
- Some experiments at high supersonic speeds on the aerodynamic and boundary-layer transition characteristics of high-drag bodies of revolution
- Investigation of boundary-layer transition on flat-faced bodies of revolution at high supersonic speeds
- Performance comparison at Mach numbers 1.8 and 2.0 of full-scale and quarter-scale translating-spike inlets
- Analysis of two-stage-turbine efficiency characteristics in terms of work and speed requirements
- Analysis of efficiency characteristics of a single-stage turbine with downstream stators in terms of work and speed requirements
- Investigation of a supersonic-inlet - turbojet-engine combination at Mach 2.0 and angles of attack up to 6 degrees
- Use of main-inlet bypass to supply ejector exhaust nozzle at supersonic speeds
- Approximate analysis of effects of large deflections and initial twist on torsional stiffness of a cantilever plate subjected to thermal stresses
- Approximate analysis of effects of large deflections and initial twist on torsional stiffness of a cantilever plate subjected to thermal stresses
- Use of constant diffuser Mach number as a control parameter for variable-geometry inlets at Mach numbers of 1.8 to 2.0
- Effect of ambient-temperature variation on the matching requirements of inlet-engine combinations at supersonic speeds
- A review of NACA research through 1954 on boron compounds as fuels for jet aircraft (Project Zip)
- A reexamination of the use of simple concepts for predicting the shape and location of detached shock waves
- Analysis of coolant flow and pressure requirements for a return-flow turbine rotor blade design using hydrogen, helium, or air as coolant
- Analytical investigation of fuel-cooled turbine blades with return-flow type of finned coolant passages
- Wind-tunnel investigation at low speeds to determine flow-field characteristics and ground influence on a model with jet-augmented flaps
- Weight-strength studies of structures representative of fuselage construction
- Normal-force and hinge-moment characteristics at transonic speeds of flap-type ailerons at three spanwise locations on a 4-percent-thick sweptback-wing-body model and pressure distribution measurements on an inboard aileron
- The erosion of meteors and high-speed vehicles in the upper atmosphere
- Basic considerations in the combustion of hydrocarbon fuels with air
- Limited heat-transfer, drag, and stability results from an investigation at Mach numbers up to 9 of a large rocket-propelled 10 degree cone
- Velocity and friction characteristics of laminar viscous boundary-layer and channel flow over surfaces with ejection or suction