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- Preliminary Data at a Mach Number of 2.40 of the Characteristics of Flap-Type Controls Equipped With Plain Overhang Balances
- A Preliminary Analysis of the Magnitude of Shock Losses in Transonic Compressors
- Experimental Static Aerodynamic Forces and Moments at High Subsonic Speeds on a Missile Model During Simulated Launching From Unswept-, Sweptback-, and Modified-Delta-Wing-Fuselage Combinations at Zero Sideslip
- Exploratory Investigation of the Effect of Wing Slots and Leading-Edge Slats on the Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing-Fuselage Configuration
- Experimental Investigation of the Oscillating Forces and Moments on a Two-Dimensional Wing Equipped With an Oscillating Circular-Arc Spoiler
- 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
- Exploratory Tests of the Behavior of Several Materials in a Supersonic Air Jet at 4,000 Degrees Fahrenheit
- Exploratory Investigation of Transpiration Cooling of a 40 Degree Double Wedge Using Nitrogen and Helium as Coolants at Stagnation Temperatures of 1,295 to 2,910 Degrees F
- Flight Investigation and Theoretical Calculations of the Fuselage Deformations of a Swept-Wing Bomber During Push-Pull Maneuvers
- Experimental Study of Heat Transfer to Small Cylinders in a Subsonic, High-Temperature Gas Stream
- Experimental Investigation of Diffuser Pressure-Ratio Control With Shock-Positioning Limit on 28-Inch Ram-Jet Engine
- Experimental Investigation of Wing-Aileron Flutter Characteristics of a 1/4-Scale Dynamic Model of the X-1E Airplane
- Some Effects of Heat Transfer at Mach Number 2.0 at Stagnation Temperatures Between 2,310 and 3,500 Degrees R on a Magnesium Fin With Several Leading-Edge Modifications
- Some Effects of Wing Height on the Vertical-Tail Pressure Distributions of a Complete Model in Sideslip at High Subsonic Speeds
- Some Examples of the Applications of the Transonic and Supersonic Area Rules to the Prediction of Wave Drag
- Review and Investigation of Unsatisfactory Control Characteristics Involving Instability of Pilot-Airplane Combination and Methods for Predicting These Difficulties From Ground Tests
- Similitude Relations for Free-Model Wind-Tunnel Studies of Store-Dropping Problems
- Preliminary Investigation of the Combustion of Pentaborane and Diborane in a Turbojet Combustor at Simulated Altitude Conditions
- Preliminary Measurements of Atmospheric Turbulence at High Altitude as Determined From Acceleration Measurements on Lockheed U-2 Airplane
- Synthesis and Hydrolysis-Rate Studies of Decaborane Derivatives
- Pentaborane Combustion Performance in 9.75-Inch-Diameter Ram-Jet Engine in Connected-Pipe Altitude Facility
- Experimental Investigation of Creep Bending and Buckling of Thin Circular Cylindrical Shells
- Strength and Ductility of Bainitic Steels
- Time-History Data of Maneuvers Performed by a Republic F-84F Airplane During Squadron Operational Training
- Tolerable Limits of Oscillatory Accelerations Due to Rolling Motions Experienced by One Pilot During Automatic-Interceptor Flight Tests
- Transonic and Supersonic Characteristics of a Horn-Balanced Control With Unbalancing Tab on a 55 Degree Sweptback Wing
- Transonic Flight Evaluation of the Effects of Fuselage Extension and Indentation on the Drag of a 60 Degree Delta-Wing Interceptor Airplane
- Transonic Flutter Investigation of a Cantilevered, Aspect-Ratio-4, 45 Degree Sweptback, Untapered Wing With Three Different Pylon-Mounted External Store Configurations
- Transonic Flutter Investigation of an All-Moveable Horizontal Tail for a Fighter Airplane
- Transonic Flutter Investigation of a 64 Degree Delta Wing Constructed With Spars Along Constant-Percent Chord Lines and Streamwise Ribs
- Transonic Flutter Investigation of Two 64 Degree Delta Wings With Simulated Streamwise Rib and Orthogonal Spar Construction
- Transonic Flutter Investigation of Arrowhead Wing With Tip Ailerons and Trailing-Edge Flaps
- Two Factors Influencing Temperature Distributions and Thermal Stresses in Structures
- The Useful Heat Capacity of Several Materials for Ballistic Nose-Cone Construction
- Reductions in Temperature-Recovery Factor Associated With Pulsating Flows Generated by Spike-Nosed Cylinders at a Mach Number of 3.50
- Recent Data on Tire Friction During Landing
- Structural Design and Engine Evaluation of an Air-Cooled Turbine Blade Composed of Corrugation and a Semistrut for Operation at a Tip Speed of 1200 Feet Per Second
- A Study of the Motion and Aerodynamic Heating of Missiles Entering the Earth's Atmosphere at High Supersonic Speeds
- Supersonic Free-Flight Measurement of Heat Transfer and Transition on a 10 Degree Cone Having a Low Temperature Ratio
- Rocket Thrust Variation With Foamed Liquid Propellants
- Rocket-Model Investigation of Hinge-Moments on a Trailing-Edge Control on a 52.5 Degree Swept Wing Between Mach Numbers of 0.70 and 1.80
- Pressure Distribution Over a Series of Related Afterbody Shapes as Affected by a Propulsive Jet at Transonic Speeds
- Pressure Measurements at Transonic and Low Supersonic Speeds on a Thin Conical Cambered Low-Aspect-Ratio Delta Wing in Combination With Basic and Indented Bodies
- Some Ground Measurements of the Forces Applied by Pilots to a Side-Located Aircraft Controller
- Some Properties of Wing and Half-Body Arrangements at Supersonic Speeds
- Transonic Wind-Tunnel Investigation of Static-Pressure Fluctuations in Duct of a Scale Inlet Model of a Supersonic Fighter-Bomber Airplane
- Transonic Wind-Tunnel Investigation of Static Longitudinal Stability and Control Characteristics and Drag of a 0.05-Scale Model of the Chance Vought XF8U-3 Airplane : TED No. NACA AD 3133
- Theoretical and Experimental Investigation of Arbitrary Aspect Ratio, Supercavitating Hydrofoils Operating Near the Free Water Surface
- Theoretical Determination of Low-Drag Supercavitating Hydrofoils and Their Two-Dimensional Characteristics at Zero Cavitation Number