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- Investigation at High Subsonic Speeds of the Static Longitudinal and Lateral Stability Characteristics of Two Canard Airplane Configurations
- Investigation of Drag and Static Longitudinal and Lateral Stability and Control Characteristics of 1/20-Scale Model of McDonnell F4H-1 Airplane at Mach Numbers of 1.57, 1.87, 2.16, and 2.53: Phase II Model
- Investigation of Static Stability and Drag Characteristics of a 1/10-Scale Model of the Avco Booster Vehicle at Mach Numbers of 1.60 and 2.00, Coord. No. AF-AM-58
- Static Longitudinal and Lateral Stability Characteristics of an 0.065-Scale Model of the Chance Vought XRSSM-N-9a (REGULUS II) Missile at Mach Numbers from 1.6 to 2.0 (TED No. NACA AD 3122)
- The Frequency Content of the Control Input and Airplane Response Obtained During Service Operations of Fighter Airplanes
- Wall Interference in a Perforated Wind Tunnel
- Study of the Micro-Nonuniformity of the Plastic Deformation of Steel
- A Theoretical Investigation of the Drag of Generalized Aircraft Configurations in Supersonic Flow
- Comparison of Combustion Reactivity of Ethyldecaborane Fuels With Typical Hydrocarbon Fuels on Basis of Spray Flammability Limits of Fuel-Rich Mists and Calculated Lean-Limit Flame Temperatures for Fuel Vapor-Air Systems
- A Second-Order Shock-Expansion Method Applicable to Bodies of Revolution Near Zero Lift
- Notes on a Large-Scale Statistical Program for the Establishment of Maneuver-Loads Design Criteria for Military Airplanes
- A Note on the Ability to Predict Transonic Drag-Rise Changes Due to Model Modifications
- Observation of Laminar Flow on an Air-Launched 15 Degree Cone-Cylinder at Local Reynolds Numbers to 50 X 10(Exp 6) at Peak Mach Number of 6.75
- Origin and Development of Leading-Edge Cracks in Turbojet Engine Buckets
- Performance of Twin-Duct Variable-Geometry Side Inlets at Mach Numbers of 1.5 to 2.0
- 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