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- Tests of the Northrop XB-62 Missile in the Ames 40- by 80-Foot Wind Tunnel
- Longitudinal Aerodynamic Characteristics to Large Angles of Attack of a Cruciform Missile Configuration at a Mach Number of 2
- Preliminary Investigation of a Technique for Stability Studies of a Self-Propelled Model of a Submerged Submarine
- The Resistance to Air Flow of Porous Materials Suitable for Boundary-Layer-Control Applications Using Area Suction
- The Small-Disturbance Method for Flow of a Compressible Fluid With Velocity Potential and Stream Function as Independent Variables
- Lift and Moment Equations for Oscillating Airfoils in an Infinite Unstaggered Cascade
- Measurement of Heat Transfer in the Turbulent Boundary Layer on a Flat Plate in a Supersonic Flow and Comparison With Skin-Friction Results
- Results of Edge-Compression on Stiffened Flat-Sheet Panels of Alclad and Nonclad 14S-T6, 24S-T3, and 75S-T6 Aluminum Alloys
- Application of Two-Dimensional Vortex Theory to the Prediction of Flow Fields Behind Wings of Wing Body Combinations at Subsonic and Supersonic Speeds
- Statistical Study of Overstressing in Steel
- Tests of Bonded and Riveted Sheet-Stringer Panels
- Span Load Distribution Resulting From Constant Vertical Acceleration for Thin Sweptback Tapered Wings With Streamwise Tips: Supersonic Leading and Trailing Edges
- Use of a Hot-Wire Anemometer in Shock-Tube Investigations
- Ion Tracer Technique for Airspeed Measurement at Low Densities
- A Method for Estimating the Effect of Turbulent Velocity Fluctuations in the Boundary Layer on Diffuser Total-Pressure-Loss Measurements
- Incompressible Flow Past a Sinusoidal Wall of Finite Amplitude
- Effect of Surface Roughness Over the Downstream Region of a 23 Degree Conical Diffuser
- Trends of Rolling-Contact Bearings as Applied to Aircraft Gas-Turbine Engines
- Thermal Conductance of Contacts in Aircraft Joints
- Theoretical and Experimental Investigation of Aerodynamic-Heating and Isothermal Heat-Transfer Parameters on a Hemispherical Nose With Laminar Boundary Layer at Supersonic Mach Numbers
- The Role of Triple Collisions in Excitation of Molecular Vibrations in Nitrous Oxide
- Time-Dependent Buckling of a Uniformly Heated Column
- Transonic Flow Past Cone Cylinders
- Viscosity Corrections to Cone Probes on Rarefied Supersonic Flow at a Nominal Mach Number of 4
- A Photographic Method for Determining Vertical Velocities of Aircraft Immediately Prior to Landing
- Review of Information on Induced Flow of a Lifting Rotor
- Manual of the ICAO Standard Atmosphere Calculations by the NACA
- Reduction of Helicopter Parasite Drag
- Electrical Analogies for Stiffened Shells With Flexible Rings
- On the Analysis of Linear and Nonlinear Dynamical Systems From Transient-Response Data
- Role of Nickel Dip in Enameling of Sheet Steel
- Rolling Effectiveness and Aileron Reversal of Rectangular Wings at Supersonic Speeds
- Stress Analysis of Circular Semimonocoque Cylinders With Cutouts by a Perturbation Load Technique
- Subsonic Edges in Thin-Wing and Slender-Body Theory
- Starting and Operating Limits of Two Supersonic Wind Tunnels Utilizing Auxiliary Air Injection Downstream of the Test Section
- A Theoretical Investigation of the Short-Period Dynamic Longitudinal Stability of Airplane Configurations Having Elastic Wings of 0 Degree to 60 Degrees Sweepback
- Evaluation of Alloys for Vacuum Brazing of Sintered Wrought Molybdenum for Elevated-Temperature Applications
- Theoretical Calculations of the Lateral Stability Derivatives for Triangular Vertical Tails with Subsonic Leading Edges Traveling at Supersonic Speeds
- Theoretical Supersonic Force and Moment Coefficients on a Sideslipping Vertical- and Horizontal-Tail Combination with Subsonic Leading Edges and Supersonic Trailing Edges
- Study of the Subsonic Forces and Moments on an Inclined Plate of Infinite Span
- Shearing-Stress Measurements by Use of a Heated Element
- Flight Investigation at Large Angles of Attack of the Static-Pressure Errors of a Service Pitot-Static Tube Having a Modified Orifice Configuration
- A Substitute-Stringer Approach for Including Shear-Lag Effects in Box-Beam Vibrations
- A Design Study of Leading-Edge Inlets for Unswept Wings
- Gust Experience of a Helicopter and an Airplane in Formation Flight
- Bending Tests on Box Beams Having Solid- and Open-Construction Webs
- Mechanical Properties at Room Temperature of Four Cermets of Titanium Carbide with Nickel Binder
- Mechanical Properties at Room Temperature of Four Cermets of Tungsten Carbide with Cobalt Binder
- Analysis of Straight Multicell Wings on Cal-Tech Analog Computer
- Buckling of Long Square Tubes in Combined Compression and Torsion and Comparison with Flat-Plate Buckling Theories