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- Correlation Between Hydrogen Pressure and Protective Action of Additives in the Molten Sodium Hydroxide - Nickel System
- Effect of an Adjustable Supersonic Inlet on the Performance Up to Mach Number 2.0 of a J34 Turbojet Engine
- Flutter Tests of a 1/25-Scale Model of the B-36J/RF-84F Tip-Coupled Airplane Configuration in the Langley 19-Foot Pressure Tunnel
- Flight Investigation of the Performance of a Two-Stage Solid-Propellant Nike-Deacon (DAN) Meteorological Sounding Rocket
- The Fatigue Strength of Riveted Joints and Lugs
- Equations and Procedures for Numerically Calculating the Aerodynamic Characteristics of Lifting Rotors
- Fatigue Tests on Notched and Unnotched Sheet Specimens of 2024-T3 and 7075-T6 Aluminum Alloys and of SAE 4130 Steel With Special Consideration of the Life Range From 2 to 10,000 Cycles
- Stability Derivatives of Cones at Supersonic Speeds
- Stability Limits and Burning Velocities of Laminar Hydrogen-Air Flames at Reduced Pressure
- Stability of Systems Containing a Heat Source - The Rayleigh Criterion
- A Review of Recent Information on Boundary-Layer Transition at Supersonic Speeds
- On a Method for Optimization of Time-Varying Linear Systems With Nonstationary Inputs
- Wing-Body Combinations With Certain Geometric Restraints Having Low Zero-Lift Wave Drag at Low Supersonic Mach Numbers
- Factors That Affect Operational Reliability of Turbojet Engines
- Free-Flight Investigation of Effects of Simulated Sonic Turbojet Exhaust on the Drag of Twin-Jet Boattail Bodies at Transonic Speeds
- Temperature Drops Through Liquid-Cooled Turbine Blades With Various Cooling-Passage Geometries
- Tensile Properties of HK31XA-H24 Magnesium-Alloy Sheet Under Rapid-Heating Conditions and Constant Elevated Temperatures
- Tentative Method for Calculation of the Sound Field About a Source Over Ground Considering Diffraction and Scattering Into Shadow Zones
- Experimental Investigation of the Strength of Multiweb Beams With Corrugated Webs
- Influence of Copper Ions on Adherence of Vitreous Coatings to Stainless Steel
- Experimental Study and Analysis of Loading and Pressure Distributions on Delta Wings Due to Thickness and to Angle of Attack at Supersonic Speeds
- An Experimental Study at High Subsonic Speeds of Several Tail Configurations on a Model with an Unswept Wing
- Influence of Hot-Working Conditions on High-Temperature Properties of a Heat-Resistant Alloy
- Effect of Design Over-All Compressor Pressure Ratio Division on Acceleration Characteristics of Three Hypothetical Two-Spool Turbojet Engines
- Mechanical Tests on Specimens From Large Aluminum-Alloy Forgings
- Evaluation of Liquefied Hydrocarbon Gases as Turbojet Fuels
- Low-Speed Longitudinal Aerodynamic Characteristics of a 45 Degree Sweptback Wing With Double Slotted Flaps
- An Investigation of Ejection Releases of Submerged and Semisubmerged Dynamically Scaled Stores from a Simulated Bomb Bay of a Fighter-Bomber Airplane at Supersonic Speeds
- Factors Controlling Air-Inlet Flow Distortions
- Characteristics of Four Nose Inlets as Measured at Mach Numbers Between 1.4 and 2.0
- Experimental Investigation of a Transonic Axial-Flow-Compressor Rotor Designed for Sonic Inlet Velocity with an Inlet Hub-Tip Radius of 0.35
- Transonic-Wind-Tunnel Investigation of the Effects of Lip Bluntness and Shape on the Drag and Pressure Recovery of a Normal-Shock Nose Inlet in a Body of Revolution
- Investigation of the Laminar Aerodynamic Heat-Transfer Characteristics of a Hemisphere-Cylinder in the Langley 11-inch Hypersonic Tunnel at a Mach Number of 6.8
- Effect of a Fuselage on the Low-Speed Longitudinal Aerodynamic Characteristics of a 45 Degree Sweptback Wing with Double Slotted Flaps
- Time-Vector Determined Lateral Derivatives of a Swept-Wing Fighter-Type Airplane with Three Different Vertical Tails at Mach Numbers Between 0.70 and 1.48
- Study of Aluminum Deformation by Electron Microscopy
- Analysis of Limitations Imposed on One-Spool Turboprop-Engine Designs by Compressors and Turbines at Flight Mach Numbers of 0.06, and 0.8
- Preliminary Investigation of a Family of Diffusers Designed for Near Sonic Inlet Velocities
- Effect of Mach Number on Boundary-Layer Transition in the Presence of Pressure Rise and Surface Roughness on an Ogive-Cylinder Body with Cold Wall Conditions
- Performance and Operational Studies of a Full-Scale Jet-Engine Thrust Reverser
- Experimental Investigation of a 0.4 Hub-Tip Diameter Ratio Axial-Flow Compressor Inlet Stage at Transonic Inlet Relative Mach Numbers 3: Effect of Tip Taper on Over-All and Blade-Element Performances
- A Theoretical Estimate of the Effects of Compressibility on the Performance of a Helicopter Rotor in Various Flight Conditions
- Mach Number Measurements and Calibrations During Flight at High Speeds and at High Altitudes Including Data for the D-558-II Research Airplane
- An Investigation of the Release Characteristics of a 1/30 Dynamically Scaled AVCO Booster Vehicle from the Simulated Bomb Bay of the B-52 Airplane : COORD. No. AF-AM-59
- Experimental Investigation of a Five-Stage Axial-Flow Research Compressor With Transonic Rotors in All Stages 3: Interstage Data and Individual Stage Performance Characteristics
- Transonic Wind-Tunnel Investigation of the Aerodynamic Loading Characteristics of a Highly Tapered Upswept Wing in the Presence of a Body With and Without Indentation
- Limited Hydrodynamic Investigation of a 1/15-Size Model of a Modified Nose-Inlet Multijet Water-Based Aircraft
- Pressure Distributions at Mach Numbers of 1.6 and 1.9 of a Conically Cambered Wing of Triangular Plan Form With and Without Pylon-Mounted Engine Nacelles
- On the Range of Applicability of the Transonic Area Rule
- Fabrication Techniques and Heat-Transfer Results for Cast-Cored Air-Cooled Turbine Blades