Browse TRAIL Inventories

Compressive and torsional buckling of thin-wall cylinders in yield region

Compressive stress-strain properties of 7075-T6 aluminum-alloy sheet at elevated temperatures

Analysis of an automatic control to prevent rolling divergence

Boundary layer behind shock or thin expansion wave moving into stationary fluid

Bodies of revolution having minimum drag at high supersonic airspeeds

Boundary-layer transition at supersonic speeds

Effect of wing camber and twist at Mach numbers from 1.4 to 2.1 on the lift, drag, and longitudinal stability of a rocket-powered model having a 52.5 degree sweptback wing of aspect ratio 3 and inline tail surfaces

Experimental and analytical investigation of an acceleration regulating control for a turbojet engine

Determination of vortex paths by series expansion technique with application to cruciform wings

A simplified method for evaluating jet-propulsion-system components in terms of airplane performance

Free-flight measurements of the zero-lift drag of several wings at Mach numbers from 1.4 to 3.8

Effect of transverse body force on channel flow with small heat addition

Effect of wing size and amount of indentation on applicability of transonic area rule to swept-wing configurations

Effectiveness of inhibitors for mass transfer and corrosion in sodium hydroxide - nickel systems

Effects of internal boundary-layer control on the performance of supersonic aft inlets

The effect of fluid injection on the compressible turbulent boundary layer : the effect of skin friction of air injected into the boundary layer of a cone at M = 2.7

An evaluation of an aeromechanical method of minimizing servo- missile transfer function variations with flight condition

Evaluation of an automatic inlet-pressure control valve for study of transient engine performance characteristics

Effects of vertical fins near the nose of the fuselage on the directional and damping-in-yaw stability derivatives of an airplane model under steady-state and oscillatory conditions

The Effects of the Addition of Small Fuselage-Mounted Fins on the Static Directional Stability Characteristics of a Model of a 45 Degree Swept-Wing Airplane at Angles of Attack up to 15.3 degrees at a Mach Number of 2.01

Effects of variations in combustion-chamber configuration on ignition delay in a 50-pound-thrust rocket

Experimental investigation of interference effects of lateral-support struts on afterbody pressures at Mach 1.9

Experimental investigation of effect of cooling air on turbine performance of two turbojet engines modified for air-cooling

Experimental investigation of the effect of boundary-layer transition on the average heat transfer to a yawed cylinder in supersonic flow

Experimental investigation of the aerodynamic loading on a helicopter rotor blade in forward flight

Aerodynamic characteristics of a 6-percent-thick symmetrical circular-arc airfoil having a 30-percent-chord trailing-edge flap at a Mach number of 6.9

Tabulated pressure data for a series of controls on a 60 degree delta wing at Mach numbers of 1.61 and 2.01

Tabulated pressure data for several flap-type trailing edge controls on a trapezoidal wing at Mach numbers of 1.61 and 2.01

Tables and charts for thermodynamic calculations involving air and fuels containing boron, carbon, hydrogen, and oxygen

Static stability characteristics of a cambered-delta-wing model at high subsonic speeds

Static-thrust characteristics of the NACA 8.75-(5)(05)-037 dual-rotation propeller

A summary of results obtained during flight simulation of several aircraft prototypes with variable-stability airplanes

Supersonic-area-rule design and rocket-propelled flight investigation of a zero-lift straight-wing-body-nacelle configuration between Mach numbers 0.8 and 1.53

Self shielding in rectangular and cylindrical geometries

Shear strength at 75 F to 500 F of fourteen adhesives used to bond a glass-fabric-reinforced phenolic resin laminate to steel

A simple method for calculating the characteristics of the Dutch roll motion of an airplane

Some observations on maximum pressure rise across shocks without boundary-layer separation on airfoils at transonic speeds

Some interference effects that influence vertical-tail loads at supersonic speeds

A study of fuel-nitric acid reactivity

A study of a symmetrical, circular, internal, compression inlet

A simulator study of some longitudinal stability and control problems of a piloted aircraft in flights to extreme altitude and high speed

Simulated flight investigation of scaled-speed elastic swept-wing bomber and fighter models coupled wing tip to wing tip

A simulation study of a wingless missile

Static lateral and directional stability and control characteristics of revised 1/22-scale model of the Republic F-105 airplane at Mach numbers of 1.41 and 2.01 : COORD No. AF-163

Static lateral and directional stability and control characteristics of a 1/15-scale model of the Grumman F11F-1 airplane at Mach numbers of 1.41, 1.61, and 2.01 : TED No. NACA DE 390

Results of a flight investigation to determine the zero-lift drag characteristics of a 60 degree delta wing with NACA 65-006 airfoil section and various double-wedge sections at Mach numbers from 0.7 to 1.6

Static longitudinal stability and control characteristics of a model of a 45 degree swept-wing fighter airplane at Mach numbers of 1.41, 1.61, and 2.01

Static stability and control characteristics of a 0.04956-scale-model of the Convair F-102A airplane at transonic speeds

Static lateral-directional stability characteristics of five contemporary airplane models from wind-tunnel tests at high subsonic and supersonic speeds

Static longitudinal and lateral stability characteristics including effects of transonic area rule and wing modification of a 0.10-scale model of the Douglas A4D-1 airplane at transonic speeds: TED No. NACA AD 3114


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