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- Preliminary investigation of hydrazine as a rocket fuel
- A comparison of the simulated-altitude performance of two turbojet combustor types
- Control during starting of gas-turbine engines
- Experimental investigation of the effects of support interference on the drag of bodies of revolution at a Mach number of 1.5
- A flight investigation and analysis of the lateral-oscillation characteristics of an airplane
- Theoretical analysis of the performance of a supersonic ducted rocket
- An investigation of the downwash and wake behind large-scale swept and unswept wings
- Vibration of turbine blades in a turbojet engine during operation
- Investigation of the diborane - hydrogen peroxide propellant combination
- Effect of three flame-holder configurations on subsonic flight performance of rectangular ram jet over range of altitudes
- Experimental investigation of thrust augmentation of 4000-pound-thrust centrifugal-flow-type turbojet engine by injection of water and alcohol at compressor inlets
- Experimental investigation of thrust augmentation of axial-flow-type 4000-pound-thrust turbojet engine by water and alcohol injection at compressor inlet
- Investigation of two pitot-static tubes at supersonic speeds
- Additional free-flight tests of the rolling effectiveness of several wing-spoiler arrangements at high subsonic, transonic, and supersonic speeds
- Ditching Tests of a 1/8-Scale Model of the Chance Vought XF6U-1 Airplane, TED No. NACA DE319
- Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine, 7, Pressure and Temperature Distributions
- Performance of conical jet nozzles in terms of flow and velocity coefficients
- Altitude-Wind-Tunnel Investigation of a 4000-Pound-Thrust Axial-Flow Turbojet Engine, Part 1, Performance and Windmilling Drag Characteristics
- Altitude-Wind-Tunnel Investigation of a 4000-Pound-Thrust Axial-Flow Turbojet Engine. 2 - Operational Characteristics
- Full-scale investigation of aerodynamic characteristics of a typical single-rotor helicopter in forward flight
- Effect of centrifugal force on the elastic curve of a vibrating cantilever beam
- Measurements in Flight of the Longitudinal-Stability Characteristics of a Republic YF-84A Airplane (Army Serial No. 45-59488) at High Subsonic Mach Numbers
- Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine 1 - Analysis of Turbine Performance
- Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine 2 - Analysis of Compressor Performance
- Altitude-Wind-Tunnel Investigation of a 4000-Pound-Thrust Axial-Flow Turbojet Engine, 4 - Analysis of Compressor Performance
- Correlation of the drag characteristics of a typical pursuit airplane obtained from high-speed wind-tunnel and flight tests
- An analytical method of estimating turbine performance
- Analysis of Effects of Inlet Pressure Losses on Performance of Axial-Flow Type Turbojet Engine
- Hydrodynamic Characteristics of an Aerodynamically Refined Planing-Tail Hull
- Determination of stresses in gas-turbine disks subjected to plastic flow and creep
- Estimation of F-3 and F-4 knock-limited performance ratings for ternary and quaternary blends containing triptane or other high-antiknock aviation-fuel blending agents
- An experimental investigation of the design variables for NACA submerged duct entrances
- Performance of Allison Model 400-C6 Turbojet-Engine Compressor, 1: Over-All Performance Characteristics of Compressor at Equivalent Impeller Speeds of 6000, 7000, and 8500 RPM
- Calibration of Air-Flow Meters for J33 Compressor Investigation
- An Investigation of the McDonnell XP-85 Airplane in the Ames 40- by 80-Foot Wind Tunnel: Pressure-Distribution Tests
- An Investigation of the McDonnell XP-85 Airplane in the Ames 40- by 80-foot Wind Tunnel. Force and Moment Tests
- Altitude-Wind-Tunnel Investigation of a 3000-Pound-Thrust Axial-Flow Turbojet Engine, 4, Operational Characteristics
- Design Data for Graphical Construction of Two-Dimensional Sharp-Edge-Throat Supersonic Nozzles
- Performance Investigations of a Large Centrifugal Compressor from an Experimental Turbojet Engine
- Altitude-Wind-Tunnel Investigation of a 4000-Pound-Thrust Axial-Flow Turbojet Engine, 3, Performance Characteristics with the High-Flow Compressor
- Simulated Altitude Performance of Combustors for the 24C Turbojet Engine. III - Performance of Rectangular-Slot Baskets, 3, Performance of Rectangular-Slot Baskets
- High-Speed Wind-Tunnel Investigation of the Longitudinal Stability and Control Characteristics of a 0.10-Scale Model of the Grumman XF9F-2 Airplane, TED No. NACA DE301
- A general small-deflection theory for flat sandwich plates
- Subsonic flow over thin oblique airfoils at zero lift
- Altitude-wind-tunnel investigation of a 4000-pound-thrust axial-flow turbojet engine VI : combustion-chamber performance
- Altitude-wind-tunnel investigation of operational characteristics of Westinghouse X24C-4B axial flow turbojet engine
- Linear theory of boundary effects in open wind tunnels with finite jet lengths
- Equations for the design of two-dimensional supersonic nozzles
- Aerodynamic characteristics at high speeds of related full-scale propellers having different blade-section cambers
- Knocking combustion observed in a spark-ignition engine with simultaneous direct and Schlieren high-speed motion pictures and pressure records