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- Theoretical performance of JP-4 fuel with a 70-30 mixture of fluorine and oxygen as a rocket propellant 2: Equilibrium composition
- Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant 2: equilibrium composition
- Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant 1: frozen composition
- Investigation of a related series of turbine-blade profiles in cascade
- Summary of subsonic-diffuser data
- Analysis of some parameters used in correlating blowing-type boundary-layer control data
- Aerodynamic heating of aircraft components
- Aerodynamic heat transfer and zero-lift of a flat windshield canopy on the NACA RM-10 research vehicle at high Reynolds numbers for a flight Mach number range from 1.5 to 3.0
- Investigation of the possibility of simplifying missile guidance systems by the use of free-floating flaps and spring-mounted control surfaces
- Effect of leading-edge geometry on boundary-layer transition at Mach 3.1
- Free-flight investigation of the control effectiveness of a differentially deflected horizontal tail at Mach numbers from 0.8 to 1.6
- Performance of a short turbojet combustor with hydrogen fuel in a quarter-annulus duct and comparison with performance in a full-scale engine
- Performance at simulated high altitudes of a prevaporizing annular turbojet combustor having low pressure loss
- Investigation of the effectiveness of boundary-layer control by blowing over a combination of sliding and plain flaps in deflecting a propeller slipstream downward for vertical take-off
- Preliminary investigation of the effectiveness of a sliding flap in deflecting a propeller slipstream downward for vertical take-off
- Subsonic wind-tunnel investigation of the effect of fuselage afterbody on directional stability of wing-fuselage combinations at high angles of attack
- Preflight and flight-test investigation of a 50-percent-magnesium 50-percent JP-4 slurry fuel in a twin engine ram-jet vehicle
- Impingement of Water Droplets on a Rectangular Half Body in a Two-Dimensional Incompressible Flow Field
- Relation of Turbojet Propulsion System Development to the Strategic Bomber Mission
- On the Permeability of Porous Materials
- Large-Scale Wind-Tunnel Tests of an Airplane Model With a 45 Degree Sweptback Wing of Aspect Ratio 2.8 With Area Suction Applied to Trailing-Edge Flaps and With Several Wing Leading-Edge Modifications
- Effect of Throat Bleed on the Supersonic Performance of a Half-Conical Side-Inlet System
- Supersonic Investigation of the Lift, Drag, Static Stability, and Hinge-Moment Characteristics of a Rocket-Powered Model of a Ballistic-Missile Configuration
- Perforated Sheets as a Porous Material for Distributed Suction and Injection
- The Subsonic Lateral and Longitudinal Static Stability Characteristics Up to Large Angles of Sideslip for a Triangular-Wing Airplane Model Having a Ventral Fin
- Some Linear Dynamics of Two-Spool Turbojet Engines
- Stall Propagation in Axial-Flow Compressors
- Space Heating Rates for Some Premixed Turbulent Propane-Air Flames
- Hydrodynamic Impact Loads in Smooth Water for a Prismatic Float Having an Angle of Dead Rise of 10 Degrees
- Generalized Tables of Corrections to Thermodynamic Properties for Nonpolar Gases
- Attenuation in a Shock Tube Due to Unsteady-Boundary-Layer Action
- A Theory for the Elastic Deflections of Plates Integrally Stiffened on One Side
- Tabulation of the F(Sub Lambda) Functions Which Occur in the Aerodynamic Theory of Oscillating Wings in Supersonic Flow
- Influence of Temperature on Creep, Stress-Rupture and Static Properties of Melamine-Resin and Silicone-Resin Glass-Fabric Laminates
- Influence of Large Amplitudes on Flexural Motions of Elastic Plates
- Thermodynamic Properties of Gaseous Nitrogen
- Time Correlator for Problems in Aerodynamics
- Effect of Carriage Mass Upon the Loads and Motions of a Prismatic Body During Hydrodynamic Impact
- Wind-Tunnel Investigation of a Number of Total-Pressure Tubes at High Angles of Attack: Subsonic, Transonic, and Supersonic Speeds
- Mechanism of Generation of Pressure Waves at Flame Fronts
- Investigation of Far Noise Field of Jets 1: Effect of Nozzle Shape
- Vapor-Phase Oxidation and Spontaneous Ignition-Correlation and Effect of Variables
- Correlation, Evaluation, and Extension of Linearized Theories for Tire Motion and Wheel Shimmy
- Linearized Lifting-Surface and Lifting-Line Evaluations of Sidewash Behind Rolling Triangular Wings at Supersonic Speeds
- Charts for Estimating Rotor-Blade Flapping Motion of High-Performance Helicopters
- A Simplified Method for Approximating the Transient Motion in Angles of Attack and Sideslip During a Constant Rolling Maneuver
- Measurement of Static Pressure on Aircraft
- Remark on the Theory of Lifting Surfaces
- On the Gas Dynamics of a Rotating Impeller
- A Flat Wing With Sharp Edges in a Supersonic Stream