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- Recovery temperatures and heat transfer near two-dimensional roughness elements at Mach 3.1
- Low-speed yawed-rolling characteristics and other elastic properties of a pair of 40-inch-diameter, 14-ply-rating, type VII aircraft tires
- Effects of ground proximity on the thrust of a simple downward-directed jet beneath a flat surface
- Effectiveness of boundary-layer control, obtained by blowing over a plain rear flap in combination with a forward slotted flap, in deflecting a slipstream downward for vertical take-off
- Simplified Method for Determination of Critical Height of Distributed Roughness Particles for Boundary-Layer Transition at Mach Numbers From 0 to 5
- Effect of Design Variables on Performance of Mach 4.0 Hydrogen Expansion Engines
- Experimental Investigation of Effect of Spike- Tip and Cowl-Lip Blunting on the Internal Performance of a Two-Cone Cylindrical-Cowl Inlet at Mach Number 4.95
- Evaluation of Some Aerodynamic Controls for a Low Aspect Ratio Missile
- Induction System Characteristics and Engine Surge Occurrence for Two Fighter-Type Airplanes
- The Effects of Body Vortices and the Wing Shock-Expansion Field on the Pitch-Up Characteristics of Supersonic Airplanes
- Correlations Among Ice Measurements, Impingement Rates Icing Conditions, and Drag Coefficients for Unswept NACA 65A004 Airfoil
- Design and Experimental Performance of a 0.35 Hub-Tip Radius Ratio Transonic Axial-Flow-Compressor Rotor Designed for 40 Pounds Per Second Per Unit Frontal Area
- The Prospects for Laminar Flow on Hypersonic Airplanes
- The Effect of Free-Stream Turbulence on Heat Transfer From a Flat Plate
- Area-Suction Boundary-Layer Control as Applied to the Trailing-Edge Flaps of a 35 Degree Swept-Wing Airplane
- Some Observations Relating to Recovery of Internal Friction During Fatigue of Aluminum
- Some Factors Affecting the Stability and Performance Characteristics of Canard Aircraft Configurations
- Theoretical Performance of Liquid Ammonia With Liquid Oxygen as a Rocket Propellant
- Theory and Experiments on Supersonic Air-to-Air Ejectors
- Turbulence and Temperature Fluctuations Behind a Heated Grid
- Turbulent Shearing Stress in the Boundary Layer of Yawed Flat Plates
- A Theoretical Study of Stagnation-Point Ablation
- Relative Motion in the Terminal Phase of Interception of a Satellite or a Ballistic Missile
- On the Statistical Theory of Turbulence
- Relation of Journal Bearing Performance to Minimum Oil-Film Thickness
- Qualitative Simulator Study of Longitudinal Stick Forces and Displacements Desirable During Tracking
- Turbulent Flow Through Porous Resistances Slightly Inclined to the Flow Direction
- Wall Pressure Fluctuations in a Turbulent Boundary Layer
- Wind-Tunnel Investigation at a Mach Number of 2.01 of Forebody Strakes for Improving Directional Stability of Supersonic Aircraft
- Two-Dimensional Diffusion Theory Analysis of Reactivity Effects of a Fuel-Plate-Removal Experiment
- Comparison of Performance of Two Aerodynamically Similar 14-Inch-Diameter Single-Stage Compressor Rotors of Different Chord Length
- Summary of Methods of Measuring Angle of Attack on Aircraft
- Low-Temperature, Vapor-Phase Oxidation of Fuel-Rich Hydrocarbon Mixtures
- Stall Propagation in a Cascade of Airfoils
- Static Longitudinal and Lateral Stability and Control Characteristics of a Model of a Swept-Wing Fighter-Bomber-Type Airplane With a Top Inlet at Mach Numbers From 1.6 to 2.35
- Study of Hydrogen Embrittlement of Iron by Internal-Friction Methods
- Water-Impact Theory for Aircraft Equipped With Nontrimming Hydro-Skis Mounted on Shock Struts
- Method of Split Rigidities and Its Application to Various Buckling Problems
- Analysis of harmonic forces produced at hub by imbalances in helicopter rotor blades
- Lightning Hazards to Aircraft Fuel Tanks
- Data From Flow-Field Surveys Behind a Large-Scale Thin Straight Wing of Aspect Ratio 3
- Flight Investigation of Effects of Retreating-Blade Stall on Bending and Torsional Moments Encountered by a Helicopter Rotor Blade
- Flight Investigation of Effects of Atmospheric Turbulence and Moderate Maneuvers on Bending and Torsional Moments Encountered by a Helicopter Rotor Blade
- Hydrodynamic Impact Loads on 30 Degree and 60 Degree V-Step Plan-Form Models With and Without Dead Rise
- Free-Flight Investigation to Determine the Inlet External Drag of Four Inlet Models at Mach Numbers From 1.50 to 3.00
- General Instability of Stiffened Cylinders
- Hydrodynamic Impact Loads of a -20 Degree Dead-Rise Inverted-V Model and Comparisons With Loads of a Flat-Bottom Model
- Experimental Evaluation of Low-Band-Pass Landing-Gear Shock Absorber for Pulse Loadings
- Free-Flight Investigation at Mach Numbers From 0.8 to 1.5 of the Effect of a Fuselage Indentation on the Zero-Lift Drag of a 52.5 Degree Sweptback-Wing-Body Configuration With Symmetrically Mounted Stores on the Fuselage
- Prandtl Number Effects on Unsteady Forced-Convection Heat Transfer