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- Investigation of a Pulse-Jet-Powered Helicopter Rotor on the Langley Helicopter Test Tower
- An Investigation of a Method for Obtaining Hydrodynamic Data at Very High Speeds With a Free Water Jet
- Investigation of a Canard Missile Configuration (NACA RM-4) in the Langley 9-Inch Supersonic Tunnel at Mach Numbers of 1.62 and 1.93
- Bibliography of NACA Reports Related to Aircraft Control and Guidance Systems January 1949 - April 1954
- Preliminary Flight Measurements of the Total-Pressure Recovery of a Split-Wing Ram-Jet Inlet at Mach Numbers From 1.4 to 3.16
- Development of Metal-Bonding Adhesives With Improved Heat-Resistant Properties
- Tables for the Computation of Wave Drag of Arrow Wings of Arbitrary Airfoil Section
- Additional Static and Fatigue Tests of High-Strength Aluminum-Alloy Bolted Joints
- Aerodynamic loads on a leading-edge flap and a leading-edge slat on the NACA 64A010 airfoil section
- Aerodynamic investigation of a four-blade propeller operating through an angle-of-attack range from 0 to 180 degrees
- Aerodynamic forces, moments, and stability derivatives for slender bodies of general cross section
- Aerodynamics of slender wings and wing-body combinations having swept trailing edges
- Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10(exp. 6) to 8.0 x 10(exp. 6)
- Airfoil section characteristics at high angles of attack
- The Ames 10- by 14-Inch Supersonic Wind Tunnel
- Aerodynamic Characteristics at High and Low Subsonic Mach Numbers of the NACA 0012, 64₂-015, and 64₃-018 Airfoil Sections at Angles of Attack from -2 Degrees to 30 Degrees
- Recovery corrections for butt-welded, straight-wire thermocouples in high-velocity, high-temperature gas streams
- Statistical survey of icing data measured on scheduled airline flights over the United States and Canada from November 1951 to June 1952
- Experimental investigation of external water-spray cooling in a turbojet engine utilizing several injection configurations including orifices in the rotor-blade bases
- Application of oblique-shock sensing system to ram-jet-engine flight Mach number control
- Static sea-level performance of an axial-flow-compressor turbojet engine with an air-cooled turbine
- A survey of methods for turbojet thrust measurement applicable to flight installation
- Combustion of aluminum borohydride in a supersonic wind tunnel
- Correlation of turbojet combustor carbon formation with smoke-volatility index, smoke point, and NACA K factor
- Transient and steady-state performance of a single turbojet combustor with four different fuel nozzles
- Average bond energies between boron and elements of the fourth, fifth, sixth, and seventh groups of the periodic table
- The rolling moment due to sideslip of swept wings at subsonic and transonic speeds
- Analysis of aerodynamic blade-loading-limit parameters for NACA 65-(C[sub zeta]₀A₁₀) 10 compressor-blade sections at low speeds
- An experimental study of a method of designing the sweptback-wing - fuselage juncture for reducing the drag at transonic speeds
- Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5
- Effect of surface roughness on characteristics of spherical shock waves
- Some observations on loss of static strength due to fatigue cracks
- Preliminary investigation of the failure of pressurized stiffened cylinders
- Summary of recent theoretical and experimental work on box-beam vibrations
- Preliminary investigation of the compressive strength and creep lifetime of 2024-T3 (formerly 24S-T3) aluminum-alloy plates at elevated temperatures
- Tensile properties of some sheet materials under rapid-heating conditions
- A study of the response of panels to random acoustic excitation
- A free-flight investigation of the effects of simulated sonic turbojet exhaust on the drag of a boattail body with various jet sizes from Mach number 0.87 to 1.50
- Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration
- Initial experimental investigation of the aerodynamic load on the wing of a model caused by a blast-induced gust that increases the angle of attack into the stall region
- Calculated effects of the lateral acceleration derivatives on the dynamic lateral stability of a delta-wing airplane
- A low-speed investigation of a thin 60©� delta wing equipped with a double slotted flap to determine the chordwise pressure distribution and the effect of vane size
- Application of nonlinear aerodynamic stability characteristics to simplify missile control and guidance systems
- Effects of an inset tab on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60©� delta wing at Mach numbers from 0.75 to 1.96
- Characteristics of loads in rough air at transonic speeds of rocket-powered models of a canard and a conventional-tail configuration
- An aerodynamic and hydrodynamic investigation of two multi-jet water-based aircraft having low transonic drag rise
- Loads associated with spoilers at supersonic speeds
- Loads on wings due to spoilers at subsonic and transonic speeds
- Vertical and drag ground-reaction forces developed in landing impacts of a large airplane
- A free-flight investigation at high subsonic and low supersonic speeds of the rolling effectiveness and drag of three spoiler controls having potentially low actuating-force requirements