Browse TRAIL Inventories

Theoretical wave drags and pressure distributions for axially symmetric open-nose bodies

Time-dependent downwash at the tail and the pitching moment due to normal acceleration at supersonic speeds

Low-speed investigation of the stalling of a thin, faired, double-wedge airfoil with nose flap

A method of determining the effect of airplane stability on the gust load factor

Method of experimentally determining radial distributions of velocity through axial-flow compressor

Effect of heat and power extraction on turbojet-engine performance 1: analytical method of performance evaluation with compressor-outlet air bleed

Effect of horizontal tail on low-speed static lateral stability characteristics of a model having 45 degree sweptback wing and tail surfaces

Effect of heat and power extraction on turbojet-engine performance 2: effect of compressor-outlet air bleed for specific modes of engine operation

Effect of heat and power extraction on turbojet-engine performance 3: analytical determination of effects of shaft-power extraction

Formulas for source, doublet, and vortex distributions in supersonic wing theory

Chart for simplifying calculations of pressure drop of a high-speed compressible fluid under simultaneous action of friction and heat transfer - application to combustion-chamber cooling passages

The interpretation of biaxial-tension experiments involving constant stress ratios

An experimental investigation of the NACA 631-012 airfoil section with leading-edge and midchord suction slots

An analysis of the normal accelerations and airspeeds of a four-engine airplane type in postwar commercial transport operations on trans-Pacific and Caribbean-South American routes

An approximate method of calculating pressures in the tip region of a rectangular wing of circular-arc section at supersonic speeds

Approximate aerodynamic influence coefficients for wings of arbitrary plan form in subsonic flow

Theoretical lift and damping in roll of thin wings with arbitrary sweep and taper at supersonic speeds : supersonic leading and trailing edges

The effects of stability of spin-recovery tail parachutes on the behavior of airplanes in gliding flight and in spins

Frequency response of positive-displacement variable stroke fuel pump

Investigation of the flow through a single-stage two-dimensional nozzle in the Langley 11-inch hypersonic tunnel

Critical stress of plate columns

Cylinder-head temperatures and coolant heat rejection of a multicylinder liquid-cooled engine of 1650-cubic-inch displacement

Comparison of theoretical and experimental heat transfer on a cooled 20 degrees cone with a laminar boundary layer at a Mach number of 2.02

A comparison of theoretical and experimental wing bending moments during seaplane landings

Effect of an unswept wing on the contribution of unswept-tail configuration to the low-speed static and rolling-stability derivatives of a midwing airplane model

Effect of aspect ratio on the air forces and moments of harmonically oscillating thin rectangular wings in supersonic potential flow

The development and performance of two small tunnels capable of intermittent operation at Mach numbers between 0.4 and 4.0

Investigation of spark-over voltage - density relation for gas-temperature sensing

Application of the wire-mesh plotting device to incompressible cascade flows

Relation Between Inflammables and Ignition Sources in Aircraft Environments

A flight investigation and analysis of the lateral-oscillation characteristics of an airplane

Stress and distortion measurements in a 45 degree swept box beam subjected to antisymmetrical bending and torsion

Stress and strain concentration at a circular hole in an infinite plate

Spectrums and diffusion in a round turbulent jet

Spin-tunnel investigation to determine the effect on spin recoveries of reducing the opening shock load of spin-recovery parachutes

The calculation of downwash behind wings of arbitrary plan form at supersonic speeds

The calculation of modes and frequencies of a modified structure from those of the unmodified structure

Theoretical analysis of various thrust-augmentation cycles for turbojet engines

Density fields around a sphere at Mach numbers 1.30 and 1.62

Maximum pitching angular accelerations of airplanes measured in flight

Gust-tunnel investigation of a wing model with semichord line swept back 60 degrees

Charts of thermodynamic properties of air and combustion products from 300 degrees to 3500 degrees R

The dynamic lateral control characteristics of airplane models having unswept wings with round-and sharp-leading-edge sections

Graphical method for obtaining flow field in two-dimensional supersonic stream to which heat is added

The effects of amount and type of camber on the variation with Mach number of the aerodynamic characteristics of a 10-percent-thick NACA 64A- series airfoil section

Properties of a boron carbide-iron ceramal

Sintering mechanism between zirconium carbide and columbium

Laminar-boundary-layer heat-transfer characteristics of a body with a pressure gradient at supersonic speeds

General method for computation of equilibrium composition and temperature of chemical reactions

Tables of thermodynamic functions for analysis of aircraft-propulsion systems


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