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- High-Speed Cascade Tests of a Blade Section Designed for Typical Hub Conditions of High-Flow Transonic Rotors
- The Hydrodynamic Force Characteristics of Streamline Bodies of Revolution Having Fineness Ratios of 6, 9, and 12 With and Without Chine Strips
- Low-Speed Wind-Tunnel Investigation of a Triangular Sweptback Air Inlet in the Root of a 45 Degree Sweptback Wing
- An Investigation of the Aerodynamic Characteristics of Thin Delta Wings With a Symmetrical Double-Wedge Section at a Mach Number of 6.9
- Investigation of Equilibrium Temperatures and Average Laminar Heat-Transfer Coefficients for the Front Half of Swept Circular Cylinders at a Mach Number of 6.9
- Investigation of the Lateral Stability Characteristics of the Douglas X-3 Configuration at Mach Numbers From 0.6 to 1.1 by Means of a Rocket-Propelled Model
- Lateral Stability Characteristics at Low Lift Between Mach Numbers of 0.85 and 1.15 of a Rocket-Propelled Model of a Supersonic Airplane Configuration Having a Tapered Wing With Circular-Arc Sections and 40 Degrees Sweepback
- Experimental Evaluation of Boron-Hydrocarbon Slurry in a 16-Inch Ram-Jet Combustor
- Flow and Force Characteristics of 2-Percent-Thick Airfoils at Transonic Speeds
- Initial Experiments on the Aerodynamic Cooling Associated With Large-Scale Vortical Motions in Supersonic Flow
- Flight Measurements of the Transonic Drag of Models of Several Isolated External Stores and Nacelles
- Flight Tests of a Delta-Wing Vertically Rising Airplane Model Powered by a Ducted Fan
- Force and Pressure Measurements on Several Canopy-Fuselage Configurations at Transonic Mach Numbers 1.41 and 2.01
- Flutter Experiences With Thin Pointed-Tip Wings During Flight Tests of Rocket-Propelled Models at Mach Numbers From 0.8 to 1.95
- Investigation at Transonic Speeds of Aerodynamic Characteristics of a Semicircular Air Inlet in the Root of a 45 Degree Sweptback Wing
- An Investigation at Supersonic Speeds of the Effect of Varying the Maximum-Thickness Position Upon the Aerodynamic Characteristics of a Series of 3 1/2-Percent-Thick Delta Wings
- Investigation of a Three-Stage Transonic Research Axial-Flow Compressor: Aerodynamic Design and Overall Performance
- Investigation of a Ramp-Type Inlet Designed for Improved Angle-of-Attack Performance at Mach Number 2.0
- Investigation of a High-Performance Axial-Flow Compressor Transonic Inlet Rotor Designed for 37.5 Pounds Per Second Per Square Foot of Frontal Area: Aerodynamic Design and Overall Performance
- Standard Atmosphere - Tables and Data for Altitudes to 65,800 Feet
- Ditching investigation of a 1/25-scale model of a 255,000-pound transport airplane
- Wind-tunnel investigation at low speed of the aerodynamic characteristics of the Army Chemical Corps model E112 bomblets
- Failure of Materials Under Combined Repeated Stresses With Superimposed Static Stresses
- Preliminary Free-Jet Performance of XRJ43-MA-3 Flight-Weight Ram-Jet Engine at Mach Numbers of 2.35, 2.50, and 2.70
- Metal-Bonding Adhesives for High-Temperature Service
- An accurate and rapid method for the design of supersonic nozzles
- Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfaces
- Acoustic analysis of ram-jet buzz
- Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 degrees to 20 degrees at high subsonic speeds
- Aerodynamic Characteristics of a Small-Scale Shrouded Propeller at Angles of Attack From 0 to 90 Degrees
- Aerodynamics of a rectangular wing of infinite aspect ratio at high angles of attack and supersonic speeds
- Amplitude of Supersonic Diffuser Flow Pulsations
- An analysis of acceleration, airspeed, and gust-velocity data from a four-engine transport airplane in operations on an eastern United States route
- An analysis of acceleration, airspeed, and gust-velocity data from one type of four-engine transport airplane operated over two domestic routes
- Acoustical Treatment for the NACA 8- by 6-Foot Supersonic Propulsion Wind Tunnel
- Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0 degrees to 180 degrees
- Analysis of behavior of simply supported flat plates compressed beyond the buckling load into the plastic range
- Analysis of accelerations, gust velocities, and airspeeds from operations of a twin-engine transport airplane on a transcontinental route from 1950 to 1952
- An analysis of accelerations, airspeeds, and gust velocities from three commercial operations of one type of medium-altitude transport airplane
- General theory of conical flows and its application to supersonic aerodynamics
- Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers 0.6 to 1.4
- Correlation of flight and analog investigations of roll coupling
- Preliminary attempts at isothermal compression of a supersonic air stream
- Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles
- Effect of diameter of closed-end coolant passages on natural-convection water cooling of gas-turbine blades
- Effect of blade-tip crossover passages on natural-convection water-cooling of gas-turbine blades
- Criteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic speeds
- Effect of a reduction in stator solidity on performance of a transonic turbine
- Visual study of free convection in a narrow vertical enclosure
- Theoretical performance of JP-4 fuel with a 70-percent-fluorine - 30-percent oxygen as a rocket propellant.