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- Performance of mixed-flow impeller, model MFI-1B, with diffuser vanes at equivalent impeller speeds from 1100 to 1700 feet per second
- Performance of five low-temperature-ratio ram-jet combustors over range of simulated altitudes
- Tests in the Ames 40- by 80-foot wind tunnel of the effects of varying wing modifications on the longitudinal characteristics of two-triangular wing airplane models with and without horizontal tails
- Matrix methods for determining the longitudinal-stability derivatives of an airplane from transient flight data
- Jet effects on pressure loading of all-movable horizontal stabilizer
- Wind pressure distributions at low lift for the XF-92A delta-wing airplane at transonic speeds
- Preliminary investigation of a technique for stability studies of a self-propelled model of a submerged submarine
- Preliminary investigation of an asymmetric swept nose inlet of circular projection at Mach number 3.85
- A preliminary study of the preparation of slurry fuels from vaporized magnesium
- Preliminary wind tunnel investigation of two types of jet-exit configurations for control of aircraft
- Preliminary investigation at subsonic and transonic speeds of the aerodynamic characteristics of a biplane composed of a sweptback and a sweptforward wing joined at the tips
- Preliminary drag measurements of the consolidated Vultee XF-92A delta-wing airplane in flight tests to a Mach number of 1.01
- Lift and drag characteristics of the Douglas X-3 research airplane obtained during demonstration flights to a Mach number of 1.20
- Lateral control characteristics of two structural similar flexible wings with 45 degrees sweep: a sweptback wing and a wing with M plan form
- Lift and drag characteristics of the Douglas D-558-II research airplane obtained in exploratory flights to a Mach number of 2.0
- Longitudinal aerodynamic characteristics to large angles of attack of a cruciform missile configuration at a Mach number of 2
- A low-speed investigation of the aerodynamic, control, and hinge-moment characteristics of two types of controls and balancing tabs on a large-scale thin delta-wing-fuselage model
- Measurement of heat-transfer and friction coefficients for flow of air in noncircular ducts at high surface temperatures
- Measurements of normal-force-coefficient fluctuation on four 9-percent-thick airfoils having different locations of maximum thickness
- Effect of ignitor design and ignitor spark-gap environment on ignition in a turbojet combustor
- Ignition of ammonia and mixed oxides of nitrogen in 200-pound-thrust rocket engines at 160 F
- Comparison of Experimental Hydrodynamic Impact Loads and Motions for a V-Step and a Transverse-Step Hydro-Ski
- On traveling waves in beams
- Comparison of normal load factors experienced with jet fighter airplanes during combat operations with those of flight tests conducted by the NACA during operational training
- Effect of channel geometry on the quenching of laminar flames
- A study of the use of controls and the resulting airplane response during service training operations of four jet fighter airplanes
- Correlation of isothermal contours formed by penetration of jet of liquid ammonia directed normal to an airstream
- Drag data for 16-inch-diameter ram-jet engine with double-cone inlet in free flight at Mach numbers from 0.7 to 1.8
- Design and test of mixed-flow impellers 4: experimental results for impeller models MF-1 and MF-2 with changes in blade height
- Effect of nozzle contour on drag of parabolic afterbodies
- Aerodynamic characteristics of several tip controls on a 60 degree wing at a Mach number of 1.61
- Aerodynamic characteristics of two flat-bottomed bodies at Mach number of 3.12
- Analytical study of losses at off-design conditions for a fixed geometry turbine
- Angle-of-attack-supersonic performance of a configuration consisting of a ramp-type scoop inlet located either on top or bottom of a body of revolution
- Analytical investigation of off-design performance of a transonic turbine
- The aerodynamic characteristics of two series of lifting bodies at Mach number 6.86
- Buffeting forces on two-dimensional airfoils as affected by thickness and thickness distribution
- Comparison of experimental with calculated results for the lifting effectiveness of a flexible 45 degree sweptback wing of aspect ratio 6.0 at Mach numbers from 0.8 to 1.3
- Comparison of effects of ailerons and combinations of spoiler-slot-deflector arrangements on spin recovery of sweptback-wing model having mass distributed along the fuselage
- Analysis of performance of four symmetrical-diagram-type subsonic inlet-stage axial-flow compressors
- Aerodynamic characteristics of several flap-type trailing-edge controls on a trapezoidal wing at Mach numbers of 1.61 and 2.01
- A comparison of flight measurements with calculations of the horizontal-tail root bending moments for a jet-powered bomber airplane
- Comparison of low-speed rotor and cascade performance for medium-camber NACA 65-(C(sub lo)A(sub 10) 10 compressor-blade sections over a wide range of rotor blade-setting angles at solidities. of 1.0 and 0.5
- Analysis of off-design operation of high Mach number supersonic turbojet engines
- Characteristics of a hydraulic control determined from transient data obtained with a turbojet engine at altitude
- Characteristics of flow about axially symmetric isentropic spikes for nose inlets at Mach number 3.85
- Combined compressor coolant injection and afterburning for turbojet thrust augmentation
- Combustion performance of two experimental turbojet annular combustors at conditions simulating high-altitude supersonic flight
- Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines II : analytical techniques
- Blow-out velocities of various petroleum, slurry, and hydride fuels in a 1 7/8-inch diameter combustor