Browse TRAIL Inventories

Investigation of Wingless Missile Configurations with Folding Controls and Low-Aspect-Ratio Stabilizing Surfaces

Investigation of two bluff shapes in axial free flight over a Mach number range from 0.35 to 2.15

A Body Modification to Reduce Drag Due to Wedge Angle of Wing with Unswept Trailing Edge

Performance of an All-internal Conical Compression Inlet With Annular Throat Bleed at Mach Number 5.0

Performance of an Inlet Having a Variable-angle Two-dimensional Compression Surface and a Fixed-geometry Subsonic Diffuser for Application to Reduced Engine Rotative Speeds- Mach Numbers 0.66, 1.5, 1.7, and 2.0

NACA Conference on High-Speed Aerodynamics A compilation of papers presented

Icing Frequencies Experienced During Climb and Descent by Fighter-Interceptor Aircraft

Combustion of gaseous hydrogen at low pressures in a 35 degree sector of a 28-inch-diameter ramjet combustor

Analysis of pressure distributions for a series of tip and trailing-edge controls on a 60 deg wing at Mach numbers of 1.61 and 2.01

Boundary-Layer-Transition Measurements in Full-Scale Flight

Effect of Pressure Level on Afterburner-wall Temperatures

Exploratory wind-tunnel investigation to determine the lift effects of blowing over flaps from nacelles mounted above the wing

Compatibility of Metals with Liquid Fluorine at High Pressures and Flow Velocities

Experimental determination of effects of frequency and amplitude on the lateral stability derivatives for a delta, a swept, and unswept wing oscillating in yaw

Systematic two-dimensional cascade tests of NACA 65-series compressor blades at low speeds

Free-Spinning-Tunnel Investigation of a 1/28-Scale Model of the North American FJ-4 Airplane with External Fuel Tanks, TED No. NACA AD 3112

Investigation of Incipient Spin Characteristics of a 1/35-Scale Model of the Convair F-102A Airplane, Coord. No. AF-AM-79

Theory of self-excited mechanical oscillations of helicopter rotors with hinged blades

A wind-tunnel investigation of the aerodynamic characteristics of a full-scale supersonic-type three-blade propeller at Mach numbers to 0.96

Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross-sectional areas

Differential equations of motion for combined flapwise bending, chordwise bending, and torsion of twisted nonuniform rotor blades

Ground simulator studies of the effects of valve friction, stick friction, flexibility, and backwash on power control system quality

Blowing-type boundary-layer control as applied to the trailing-edge flaps of a 35 degree swept-wing airplane

Flight measurements of the vibration experienced by a tandem helicopter in transition, vortex-ring state, landing, approach, and yawed flight

A flight-test study of total-pressure distortion in a thick-lipped nose inlet

Flutter analysis of rectangular wings of very low aspect ratio

Some numerical solutions of similarity equations for three-dimensional laminar incompressible boundary-layer flows

Full-scale wind-tunnel tests of a 35 degree sweptback-wing airplane with blowing from the shroud ahead of the trailing-edge flaps

Internal-friction study of aluminum alloy containing 4 weight percent copper

Internal characteristics and performance of several jet deflectors at primary-nozzle pressure ratios up to 3.0

Experimental investigation of flutter and divergence characteristics of the rocket-motor fin of the ASROC missile: COORD. No. N-AM-66

Internal characteristics and performance of an aerodynamically controlled, variable-discharge convergent nozzle

A method for rapid selection of design characteristics of 1-, 1 1/2-, and 2-stage turbines with optimum annulus taper

Investigation of the aerodynamic characteristics of a model of a supersonic bomber configuration with a swept and an unswept wing at Mach numbers from 1.79 to 2.67

Investigation of two-stage counterrotating compressor IV : over-all performance of compressor with modified second-stage rotor

An investigation of supersonic store interference in the vicinity of a 22 degree swept-wing-fuselage configuration at Mach numbers of 1.61 and 2.01

An investigation of some phenomena relating to aural detection of airplanes

A method for the calculation of wave drag on supersonic-edged wings and biplanes

A method for the calculation of the lateral response of airplanes to random turbulence

Exploratory wind-tunnel investigation at high subsonic and transonic speeds of jet flaps on unswept rectangular wings

A phenomenological relation between stress, strain rate, and temperature for metals at elevated temperatures

Performance of multiple jet-exit installations

Performance of five short multielement turbojet combustors for hydrogen fuel in quarter-annulus duct

Performance of JP-4 fuel with fluorine-oxygen mixtures in 1000-pound-thrust rocket engines

A nonlinear theory for predicting the effects of unsteady laminar, turbulent, or transitional boundary layers on the attenuation of shock waves in a shock tube with experimental comparison

Noise survey under static conditions of a turbine-driven full-scale modified supersonic propeller with an advance ratio of 3.2

Natural convection inside a flat rotating container

Effect of the proximity of the wing first-bending frequency and the short-period frequency on the airplane dynamic-response factor

Preliminary survey of possible methods for hypersonic aircraft

A preliminary study of the effect of boric oxide deposits on the performance of two selected turbine stator-blade shapes


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