Browse TRAIL Inventories

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


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