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- On the Instability of Methods for the Integration of Ordinary Differential Equations
- Tests to Determine the Adhesive Power of Passenger-Car Tires
- Flow of Gas Through Turbine Lattices
- Adaptation of Combustion Principles to Aircraft Propulsion Volume 2: Combustion in Air-Breathing Jet Engines
- The Aerodynamic Characteristics in Pitch of a 1/15-Scale Model of the Grumman F11F-1 Airplane at Mach Numbers of 1.41, 1.61, and 2.01, TED No. NACA DE 390
- Safeguards Against Flutter of Airplanes
- Free-Spinning and Recovery Characteristics of a 1/19-Scale Model of the North American T-28C Airplane, TED No. NACA AD 3127
- Effects of Intermittent Versus Continuous Heating upon the Tensile Properties of 2024-T4, 6061-T6 and 7075-T6 Alloys
- Finite Span Wings in Compressible Flow
- Flat Plate Cascades at Supersonic Speed
- On the Contribution of Turbulent Boundary Layers to the Noise Inside a Fuselage
- Fatigue-Crack Propagation in Aluminum Alloy Box Beams
- Supersonic flow past nonlifting bumped and indented bodies of revolution
- Static lateral stability and control characteristics of a model of a 45 degree swept-wing fighter airplane with various vertical tails at Mach numbers of 1.41, 1.61, and 2.01
- Aircraft configurations developing high lift-drag ratios at high supersonic speeds
- 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