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- Performance of Inconel 739 Buckets in J33-9 Turbojet Engine
- Experimental Results From a Test in Rough Air at High Subsonic Speeds of a Tailless Rocket Model Having Cruciform Triangular Wings, and a Note on the Calculation of Mean Square Loads of Aircraft in Continuous Rough Air
- Experimental Transonic Flutter Characteristics of an Untapered, 45 Degree Sweptback, Aspect Ratio 4 Wing
- An Experimental Investigation of the Effects of Several Diffusers and Diffuser-Entrance-Mixing-Section Combinations on the Power Requirements of a 4 1/2-Inch by 4 1/2-Inch Slotted Transonic Wind Tunnel
- Exploratory Investigation of the Use of Area Suction to Eliminate Air-Flow Separation in Diffusers Having Large Expansion Angles
- External-Store Drag Reduction at Transonic and Low Supersonic Mach Numbers by Application of Baldwin's Moment-of-Area Rule
- Exploratory Materials and Missile-Nose-Shape Tests in a 4,000 Degrees F Supersonic Air Jet
- Exploratory Investigation of a Helicopter Pressure-Jet System on the Langley Helicopter Test Tower
- Experimental Measurements of Forces and Moments on a Two-Dimensional Oscillating Wing at Subsonic Speeds
- Experimental Investigation of Turbine Stator-Blade-Outlet Boundary-Layer Characteristics and a Comparison With Theoretical Results
- Experimental Steady-State Yawing Derivatives of a 60 Degree Delta-Wing Model as Affected by Changes in Vertical Position of the Wing and in Ratio of Fuselage Diameter to Wing Span
- Experimental Investigation of Marquardt Shock-Positioning Control Unit on a 28-Inch Ram-Jet Engine
- Some Effects of Roll Rate on the Longitudinal Stability Characteristics of a Cruciform Missile Configuration as Determined From Flight Test for a Mach Number Range of 1.1. To 1.8
- Some Effects of Wing Fences on the Lateral Stability Derivatives of a 60 Degree Delta Wing Oscillating Continuously in Yaw
- Some Measurements of Aerodynamic Forces and Moments at Subsonic Speeds on a Wing-Tank Configuration Oscillating in Pitch About the Wing Midchord
- Some Wind-Tunnel Experiments on Single-Degree-of-Freedom Flutter of Ailerons in the High Subsonic Speed Range
- Preliminary Report on Experimental Investigation of Engine Dynamics and Controls for a 48-Inch Ram-Jet Engine
- Preliminary Measurements of the Aerodynamic Yawing Derivatives of a Triangular, a Swept, and an Unswept Wing Performing Pure Yawing Oscillations, With a Description of the Instrumentation Employed
- Tabulation of Mass-Flow Parameters for Use in Design of Turbomachine Blade Rows for Ratios of Specific Heats of 1.3 and 1.4
- Comparison of the Minimum Drag of Two Versions of a Modified Delta-Wing Fighter as Obtained From Flight Tests of Rocket-Boosted Models and Equivalent Bodies Between Mach Numbers of 0.80 and 1.64
- Turbojet Performance and Operation at High Altitudes With Hydrogen and JP-4 Fuels
- Turbulent and Laminar Heat-Transfer Measurements on a 1/6-Scale NACA RM-10 Missile in Free Fight to Mach Number of 4.2 and to a Wall Temperature of 1400 Degrees R
- Transonic Aerodynamic Characteristics of a 1/15-Scale Model of the Convair B-58 Airplane
- Turbulent-Heat-Transfer Measurements at a Mach Number of 3.90
- The Use of Area Suction for Improving the Longitudinal Characteristics of a Thin Unswept Wing-Fuselage Model With Leading- and Trailing-Edge Flaps
- Two Experiments on Applications of the Transonic Area Rule to Asymmetric Configurations
- Results of Rocket Model Test of an Airplane Configuration Having an Arrow Wing and Slender Flat-Sided Fuselage: Lift, Drag, Longitudinal Stability, Lateral Force, and Jet Effects at Mach Numbers Between 1.0 and 2.3
- Static Shear Strength of 2117-T4 (A17S-T4) Aluminum-Alloy Rivets at Elevated Temperatures
- The Subsonic Lateral and Longitudinal Static Stability Characteristics Up to Large Angles of Sideslip for a Triangular-Wing Airplane Model Having a Ventral Fin
- Supersonic Investigation of the Lift, Drag, Static Stability, and Hinge-Moment Characteristics of a Rocket-Powered Model of a Ballistic-Missile Configuration
- A Semiempirical Procedure for Estimating Wing Buffet Loads in the Transonic Region
- A Semigraphical Method for the Determination of the Rolling Characteristics of Rolleron-Equipped Missiles
- Pressure Distributions on Four Canopy-Fuselage Configurations at Transonic Speeds
- Some Effects of Sweep and Aspect Ratio on the Transonic Flutter Characteristics of a Series of Thin Cantilever Wings Having a Taper Ratio of 0.6
- Some Effects of Sweep and Thickness on the Experimental Downwash Characteristics at Transonic Speeds of a Series of Highly Tapered Wings With an Aspect Ratio of 3: Transonic Bump Method
- Some Notes on the Violent Lateral-Longitudinal Coupling Motions of the Douglas X-3 Airplane in Aileron Rolls
- The Static and Dynamic-Rotary Stability Derivatives at Subsonic Speeds of an Airplane Model With an Unswept Wing and a High Horizontal Tail
- A Transonic Wind-Tunnel Investigation of Store and Horizontal-Tail Loads and Some Effects of Fuselage-Afterbody Modifications on a Swept-Wing Fighter Airplane
- Use of Shadowgraph Technique in the Analysis of the Performance of Two Supersonic Axial-Flow Compressor Rotors Operating Over a Mean Radius Relative Inlet Mach Number Range of 0.85 to 1.7
- Wind-Tunnel Investigation of a Ram-Jet Model Having a Wing and Canard Surfaces of Delta Plan Form With 70 Degrees Swept Leading Edges: Force and Moment Characteristics at Combined Angles of Pitch and Sideslip for Mach Number 2.01
- Wind-Tunnel Investigation at High Subsonic Speeds of Some Effects of Fuselage Cross-Section Shape and Wing Height on the Static Longitudinal and Lateral Stability Characteristics of a Model Having a 45 Degree Swept Wing
- The Variation With Wing Aspect Ratio of Flap Effectiveness on Thin Rectangular Wings at Transonic Speeds
- Wind-Tunnel Investigation at Low Speed of Effects of Sideslip on Static Longitudinal Trim and Static Lateral Stability Characteristics of Three Fighter-Type Airplane Models
- Wind-Tunnel Investigation at Mach Numbers From 0.8 to 1.4 of Static Longitudinal and Lateral-Directional Characteristics of an Unswept-Wing Airplane Model
- Wind-Tunnel Investigation at Transonic Speeds of a Jet Control on a 35 Degree Swept Wing: Transonic-Bump Method
- A Transonic Investigation of Changing Indentation Design Mach Number on the Aerodynamic Characteristics of a 45 Degree Sweptback-Wing-Body Combination Designed for High Performance
- Transonic Investigation of the Effectiveness and Loading Characteristics of a Flap-Type Aileron With and Without Paddle Balances of an Unswept-Wing-Fuselage Model
- Transonic Wind-Tunnel Investigation of Static Longitudinal Force and Moment Characteristics of Two Wing-Body Combinations With Clipped-Tip and Full Delta Wings of Aspect Ratio 1.73
- A Transonic Investigation of the Static Longitudinal-Stability Characteristics of a 45 Degree Sweptback Wing-Fuselage Combination With and Without Horizontal Tail
- Transonic Wind-Tunnel Investigation of the Effects of a Heated Propulsive Jet on the Pressure Distribution Along a Fuselage Overhang