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- Effect of fuels on screaming in 200-pound-thrust liquid-oxygen - fuel rocket engine
- Wing loads and load distributions throughout the lift range of the Douglas X-3 research airplane at transonic speeds
- Preliminary survey of compressor rotor-blade wakes and other flow phenomena with a hot-wire anemometer
- Problems of performance and heating of hypersonic vehicles
- Probability and frequency characteristics of some flight buffet loads
- Preliminary free-flight study of the drag and stability of a series of short-span missiles at Mach numbers from 0.9 to 1.3
- Pressure distribution and aerodynamic loadings for several-flap-type trailing-edge controls on a trapezoidal wing at Mach numbers of 1.61 and 2.01
- Presentation on facility problems in high-temperature structures research
- Preliminary wind-tunnel tests of triangular and rectangular wings in steady roll at Mach numbers of 1.62 and 1.92
- Lateral-Stability Flight Test of a 0.125-Scale Rocket-Propelled Model of the Mcdonnell F-101A Airplane at Mach Numbers from 1.0 to 1.9
- Lift and drag of the Bell X-5 research airplane in the 45 degree sweptback configuration at transonic speeds
- Longitudinal characteristics of an unswept-wing fighter-type model with external stores at a Mach number of 1.82 and some effects of horizontal-tail and yaw-damper-vane deflection on the sideslip derivatives
- Longitudinal and lateral stability characteristics of a low-aspect-ratio unswept-wing airplane model at Mach numbers of 1.82 and 2.01
- Longitudinal stability characteristics of the Convair YF-102 airplane determined from flight tests
- A low-speed experimental investigation of the effect of a sandpaper type of roughness on boundary-layer transition
- Measurements of atmospheric turbulence over a wide range of wavelength for one meteorological condition
- Measurements of boundary-layer transition at low speed on two bodies of revolution in a low-turbulence wind tunnel
- Measurement of the longitudinal moment of inertia of a flexible airplane
- Evaporation of JP-5 fuel sprays in air streams
- Effects of two trailing-edge controls on the aerodynamic characteristics of a rectangular wing and body combination at Mach numbers from 3.00 and 5.05
- Lift, drag, and static longitudinal stability characteristics of configurations consisting of three triangular wing panels and a body of equal length at Mach numbers from 3.00 to 6.28
- A preliminary investigation of the static stability characteristics of four airplane-like configurations at Mach numbers from 3.00 to 6.28
- Exploratory investigation at a Mach number of 5.20 of the longitudinal aerodynamic characteristics of flat-bottom bodies
- Further investigation of the feasibility of the freeze-casting method for forming full-size infiltrated titanium carbide turbine blades
- Fuselage side inlets : a study of some factors affecting their performance and a comparison with nose inlets
- Impingement of water droplets on a rectangular half body in a two-dimensional incompressible flow field
- Friction studies of graphite and mixtures of graphite with several metallic oxides and salts at temperatures to 1000 F
- Heat-transfer measurements on two bodies of revolution at a Mach number of 3.12
- Heat-Requirements for Ice Protection of a Cyclically Gas-Heated, 36 Degree Swept Airfoil with Partial-Span Leading-Edge Slat
- Heat-capacity measurements of titanium and of a hydride of titanium for temperatures from 4 to 15 K including a detailed description of a special adiabatic specific-heat calorimeter
- Use of effective momentum thickness in describing turbine rotor-blade losses
- On the permeability of porous materials
- Full-scale wind-tunnel tests of the longitudinal stability and control characteristics of the XV-1 convertiplane in the autorotating flight range
- Distribution of normal component of induced velocity in lateral plane of a lifting rotor
- The effect of conical camber on the static longitudinal, lateral, and directional characteristics of a 45-degree sweptback wing at Mach numbers up to 0.96
- Effect of concentration on ignition delays for various fuel-oxygen-nitrogen mixtures at elevated temperatures
- Correlation of creep-buckling tests with theory
- Drag coefficients for droplets and solid spheres in clouds accelerating in airstreams
- Drag at model trim lift of a 1/15-scale Convair B-58 supersonic bomber
- The use of perforated inlets for efficient supersonic diffusion
- Design and test of mixed-flow impellers 7: experimental results for parabolic-bladed impeller with alternate blades cut back to form splitter vanes
- Analytical investigation of factors affecting the performance of single-stage turbines having rotor-tip discharge of cooling air
- Analytical investigation of single-stage-turbine efficiency characteristics in terms of work and speed requirements
- Aerodynamic control of supersonic inlets for optimum performance
- Calculated reactivity of uranyl-fluoride - water criticality experiments
- Analytical determination of the natural coupled frequencies and mode shapes and the response to oscillating forcing functions of tandem helicopters
- Transition-flight tests of a model of a low-wing transport vertical-take-off airplane with tilting wing and propellers
- Aerodynamic damping at Mach numbers of 1.3 and 1.6 of a control surface on a two-dimensional wing by a free-oscillation method
- Aerodynamic design of axial-flow compressors Volume 1
- Bending tests of ring-stiffened circular cylinders