TRAIL - Technical Report Archive and Image Library

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

Longitudinal and Lateral Stability, Control Characteristics, and Vertical-Tail-Load Measurements for 0.03-Scale Model of the Avro CF-105 Airplane at Mach Number 1.41

Concluding Report on Free-Spinning and Recovery Characteristics of a 1/24-Scale Model of the Grumman F11F-1 Airplane, TED No. NACA AD 395

Ditching Investigation of a 1/12-Scale Model of the Douglas F4D-1 Airplane, TED No. NACA DE 384

An Experimental Investigation of Sting-Support Effects on Drag and a Comparison with Jet Effects at Transonic Speeds

Lift, Drag, Static Stability, and Buffet Boundaries of a Model of the McDonnell F3H-1N Airplane at Mach Numbers from 0.40 to 1.27, TED No. NACA DE 351

Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches

An investigation of the hydrodynamic characteristics of a dynamic model of a transonic seaplane design having a planing-tail hull

Low-speed static stability characteristics of a cambered-delta-wing model

Lift-curve slopes determined in flight on a flexible swept-wing jet bomber

Investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections

Free-flight investigation at transonic speeds of the stability characteristics of a tailless missile configuration having a 45 degree sweptback wing of aspect ratio 4

Free-flight investigation over a Mach number range from 0.74 to 1.43 at lift coefficients from minus 0.15 to 0.75 of an airplane-configuration model having a 52.5 degree delta wing and a low swept horizontal tail

Free-flight investigation at transonic speeds of drag coefficients of a boattail body of revolution with a simulated turbojet exhaust issuing at the base from conical short-length ejectors

A free-flight investigation of the effects of a sonic jet on the total-drag and base-pressure coefficients of a boattail body of revolution from Mach number 0.83 to 1.70

Tensile properties of AZ31A-0 magnesium-alloy sheet under rapid-heating and constant-temperature conditions

Tensile properties of Inconel and RS-120 titanium-alloy sheet under rapid-heating and constant-temperature conditions

Cloud-droplet ingestion in engine inlets with inlet velocity ratios of 1.0 and 0.7

Comparison of theoretical stresses and deflections of multicell wings with experimental results obtained from plastic models

Effects of Reynolds number and leading-edge shape on the low-speed longitudinal stability of a 6-percent-thick 45 degree sweptback wing

Charts adapted from Van Driest's turbulent flat-plate theory for determining values of turbulent aerodynamic friction and heat-transfer coefficients

Effects of leading-edge radius on the longitudinal stability characteristics of two 60 degree sweptback wings at high Reynolds numbers

On possible similarity solutions for three-dimensional incompressible laminar boundary layers 2: similarity with respect to stationary polar coordinates

Wind-tunnel investigation of the damping in roll of the Bell X-1E research airplane and its components at supersonic speeds

Wind-tunnel investigation of the damping in roll of the Bell X-1A research airplane and its components at supersonic speeds

Wind-tunnel investigation of the damping in roll of the Douglas D-558-II research airplane and its components at supersonic speeds

On possible similarity solutions for three-dimensional incompressible laminar boundary layers 1: similarity with respect to stationary rectangular coordinates

Analysis of particle motions for a class of three-dimensional incompressible laminar boundary layers

Cross flows in laminar incompressible boundary layers

Comparison of flight and wind-tunnel measurements of high-speed-airplane stability and control characteristics

Qualitative study of flow characteristics through single-stage turbines as made from rotor-exit surveys

A description of the Ames 2- by 2-foot transonic wind tunnel and preliminary evaluation of wall interference

Wind-tunnel tests of blowing boundary-layer control with jet pressure ratios up to 9.5 on the trailing-edge flaps of a 35 degree sweptback wing airplane

A study of the high-speed performance characteristics of 90 degrees bends in circular ducts

A study of the efficiency of high-strength, steel, cellular-core sandwich plates in compression

Preliminary investigation of methods to increase base pressure of plug nozzles at Mach 0.9

Theoretical performance of JP-4 fuel with a 70-30 mixture of fluorine and oxygen as a rocket propellant 2: Equilibrium composition

Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant 2: equilibrium composition

Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant 1: frozen composition

Investigation of a related series of turbine-blade profiles in cascade

Summary of subsonic-diffuser data

Analysis of some parameters used in correlating blowing-type boundary-layer control data

Aerodynamic heating of aircraft components

Aerodynamic heat transfer and zero-lift of a flat windshield canopy on the NACA RM-10 research vehicle at high Reynolds numbers for a flight Mach number range from 1.5 to 3.0

Investigation of the possibility of simplifying missile guidance systems by the use of free-floating flaps and spring-mounted control surfaces

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