Browse TRAIL Inventories

An Investigation at Supersonic Speeds of the Effect of Varying the Maximum-Thickness Position Upon the Aerodynamic Characteristics of a Series of 3 1/2-Percent-Thick Delta Wings

Investigation of a Three-Stage Transonic Research Axial-Flow Compressor: Aerodynamic Design and Overall Performance

Investigation of a Ramp-Type Inlet Designed for Improved Angle-of-Attack Performance at Mach Number 2.0

Investigation of a High-Performance Axial-Flow Compressor Transonic Inlet Rotor Designed for 37.5 Pounds Per Second Per Square Foot of Frontal Area: Aerodynamic Design and Overall Performance

Standard Atmosphere - Tables and Data for Altitudes to 65,800 Feet

Ditching investigation of a 1/25-scale model of a 255,000-pound transport airplane

Wind-tunnel investigation at low speed of the aerodynamic characteristics of the Army Chemical Corps model E112 bomblets

Failure of Materials Under Combined Repeated Stresses With Superimposed Static Stresses

Preliminary Free-Jet Performance of XRJ43-MA-3 Flight-Weight Ram-Jet Engine at Mach Numbers of 2.35, 2.50, and 2.70

Metal-Bonding Adhesives for High-Temperature Service

An accurate and rapid method for the design of supersonic nozzles

Acoustic radiation from two-dimensional rectangular cutouts in aerodynamic surfaces

Acoustic analysis of ram-jet buzz

Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 degrees to 20 degrees at high subsonic speeds

Aerodynamic Characteristics of a Small-Scale Shrouded Propeller at Angles of Attack From 0 to 90 Degrees

Aerodynamics of a rectangular wing of infinite aspect ratio at high angles of attack and supersonic speeds

Amplitude of Supersonic Diffuser Flow Pulsations

An analysis of acceleration, airspeed, and gust-velocity data from a four-engine transport airplane in operations on an eastern United States route

An analysis of acceleration, airspeed, and gust-velocity data from one type of four-engine transport airplane operated over two domestic routes

Acoustical Treatment for the NACA 8- by 6-Foot Supersonic Propulsion Wind Tunnel

Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0 degrees to 180 degrees

Analysis of behavior of simply supported flat plates compressed beyond the buckling load into the plastic range

Analysis of accelerations, gust velocities, and airspeeds from operations of a twin-engine transport airplane on a transcontinental route from 1950 to 1952

An analysis of accelerations, airspeeds, and gust velocities from three commercial operations of one type of medium-altitude transport airplane

General theory of conical flows and its application to supersonic aerodynamics

Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers 0.6 to 1.4

Correlation of flight and analog investigations of roll coupling

Preliminary attempts at isothermal compression of a supersonic air stream

Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles

Effect of diameter of closed-end coolant passages on natural-convection water cooling of gas-turbine blades

Effect of blade-tip crossover passages on natural-convection water-cooling of gas-turbine blades

Criteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic speeds

Effect of a reduction in stator solidity on performance of a transonic turbine

Visual study of free convection in a narrow vertical enclosure

Theoretical performance of JP-4 fuel with a 70-percent-fluorine - 30-percent oxygen as a rocket propellant.

Turbojet combustor performance with injection of hydrogen peroxide for thrust augmentation

Internal performance characteristics of short convergent-divergent exhaust nozzles designed by the method of characteristics

An analog study of a shock-position diffuser control on a supersonic turbojet engine

Some recent research on the handling qualities of airplanes

Dynamics of a supersonic inlet with adjustable bypass in combination with a J34 turbojet engine

Flight determination of drag and pressure recovery of two scoop inlets located at maximum-body-diameter station at Mach numbers from 0.8 to 1.8

The use of the horizontal tail for roll control

Factors affecting the maximum lift-drag ratio at high supersonic speeds

Spinning and related problems at high angles of attack for high-speed airplanes

Effects of wing-body geometry on the lateral-flow angularities at subsonic speeds

A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver

Flutter investigation at low speed of a 40 degree sweptback wing with pylon-mounted stores, tested as a semispan-cantilever wing and as a full-span wing on a towed airplane model

A wind-tunnel investigation of the development of lift on wings in accelerated longitudinal motion

Wind-tunnel investigation of damping in roll at supersonic speeds of triangular wings at angles of attack

A variable-geometry annular cascade-type inlet at Mach numbers of 1.9 and 3.05


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