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- The Similarity Rules for Second-Order Subsonic and Supersonic Flow
- Sidewash in the Vicinity of Lifting Swept Wings at Supersonic Speeds
- Internal Performance of Two-Dimensional Wedge Exhaust Nozzles
- On Stokes' Stream Function in Compressible Small-Disturbance Theory
- Flight Investigation of the Low-Speed Characteristics of a 35 Degree Swept-Wing Airplane Equipped with an Area-Suction Ejector Flap and Various Wing Leading-Edge Devices
- Compressive Stress-Strain Properties of 17-7 PH and AM 350 Stainless-Steel Sheet at Elevated Temperatures
- Elliptic Cones Alone and with Wings at Supersonic Speeds
- Effects of Horizontal-Tail Position and a Wing Leading-Edge Modification Consisting of a Full-Span Flap and a Partial-Span Chord-Extension on the Aerodynamic Characteristics in Pitch at High Subsonic Speeds of a Model With a 45 Degree Sweptback Wing
- Investigation of Some Mechanical Properties of Thermenol Compressor Blades
- Experimental Investigation of Temperature Feedback Control Systems Applicable to Turbojet-Engine Control
- Experimental Comparison of Speed: Fuel-Flow and Speed-Area Controls on a Turbojet Engine for Small Step Disturbances
- Flight Investigation of the Transonic Longitudinal and Lateral Handling Qualities of the Douglas X-3 Research Airplane
- Investigation at Mach Numbers to 1.04 of Blade-Loading Characteristics of Two Full-Scale Three-Blade Supersonic Propellers Differing in Blade-Section Camber
- Tables of Characteristic Functions for Solving Boundary-Value Problems of the Wave Equation with Application to Supersonic Interference
- Effects of Some Configuration Changes on Afterburner Combustion Performance
- A Semiempirical Correlation of Afterburner Combustion Efficiency and Lean-Blowout Fuel-Air-Ratio Data with Several Afterburner-Inlet Variables and Afterburner Lengths
- Flight-Test Investigation on the Langley Control-Line Facility of a Model of a Propeller-Driven Tail-Sitter-Type Vertical-Take-Off Airplane with Delta Wing During Rapid Transitions
- Effect of Transient Heating on Vibration Frequencies of Some Simple Wing Structures
- Effects of Jet Exhausts on Flight-Determined Longitudinal and Lateral Dynamic Stability Characteristics of the Douglas D-558-II Research Airplane
- Dynamic Longitudinal Stability Characteristics of a Swept-Wing Fighter-Type Airplane at Mach Numbers Between 0.36 and 1.45
- Experimental Investigation of a 0.4 Hub-Tip Diameter Ratio Axial-Flow Compressor Inlet Stage at Transonic Inlet Relative Mach Numbers 4: Performance of Tapered-Tip Rotor Configuration with Reset Blade Angles
- Instrument Flight Trials with Helicopter Stabilized in Attitude About Each Axis Individually
- Three-Degree-of Freedom Evaluation of the Longitudinal Transfer Functions of a Supersonic Canard Missile Configuration Including Changes in Forward Speed
- Analysis of Limitations Imposed on One-Spool Ducted-Fan-Engine Designs by Compressors and Turbines at Flight Mach Numbers of 0, 0.6, and 0.8
- Experimental Investigation of a Five-Stage Axial-Flow Research Compressor with Transonic Rotors in All Stages 4: Blade-Element Performance
- High-Altitude Performance of J71-A-11 Turbojet Engine and Its Components Using JP-4 and Gaseous-Hydrogen Fuels
- Preliminary Investigation of the Effect of Surface Treatment on the Strength of a Titanium Carbide - 30 Percent Nickel Base Cermet
- Some Aspects of Fail-Safe Design of Pressurized Fuselages
- Bursting Strength of Unstiffened Pressure Cylinders with Slits
- Hinge-Moment and Effectiveness Characteristics of an Aspect-Ratio-8.2 Flap-Type Control on a 60 Degree Delta Wing at Mach Numbers from 0.72 to 1.96
- Experimental Investigation of Modified Cast-Cored Blades Having Hollow Tip Sections
- Effect of Fluid-System Parameters on Starting Flow
- Measurements of Runway Roughness of Four Commercial Airports
- Analysis of Static Aeroelastic Behavior of Low-Aspect-Ratio Rectangular Wings
- Experimental investigation of the simulation of atmospheric entry of ballistic missiles
- Performance at High Temperatures and Pressures of an Annular Turbojet Combustor Having Articulated Liner Walls
- Performance of a Supersonic Ramp-type Side Inlet With Ram-scoop Throat Bleed and Varying Fuselage Boundary-layer Removal Mach Number Range 1.5 to 2.0
- Performance of Twin-Duct Variable-Geometry Side Inlets at Mach Numbers of 1.5 to 2.0
- Preliminary Evaluation of the Wing Leading Edge as a Missile-Mounting Location
- Experimental Static Aerodynamic Forces and Moments at High Subsonic Speeds on a Canard Missile During Simulated Launching From the Midsemispan Location of a 45 Degree Sweptback Wing-Fuselage-Pylon Combination at Zero Sideslip
- A Flight and Analog Study of the Effect of Elevating the Radar-Boresight Axis Upon Stability and Tracking Performance of an Automatically Controlled Interceptor
- Flight Investigation at Low Angles of Attack to Determine the Longitudinal Stability and Control Characteristics of a Cruciform Canard Missile Configuration With a Low-Aspect-Ratio Wing and Blunt Nose at Mach Numbers From 1.2 to 2.1
- Factors Affecting Loads at Hypersonic Speeds
- Experimental Investigation of Diffuser Pressure Ratio Control With Shock Positioning Limit on 28 Inch Ram-Jet Engine
- A Review of NACA Research Through 1954 on Boron Compounds as Fuels for Jet Aircraft (Project Zip)
- Synthesis and Hydrolysis-Rate Studies of Decaborane Derivatives
- Design and Performance of Fuel Control for Aircraft Hydrogen Fuel System
- Transonic Flight Evaluation of the Effects of Fuselage Extension and Indentation on the Drag of a 60-Degree Delta Wing Interceptor Airplane
- Transonic Flutter Characteristics of a Cambered A-Plan-Form Wing With and Without Simulated Nacelles
- Results of the Flight Test of a 0.13-Scale Rocket-Boosted Model of the McDonnell F4H-1 Airplane Between Mach Numbers of 0.20 and 1.90