Browse TRAIL Inventories

Elastic and plastic buckling of simply supported metalite type sandwich plates in compression

Recommended Values of Meteorological Factors to Be Considered in the Design of Aircraft Ice-Prevention Equipment

Effect of increase in afterbody length on the hydrodynamic qualities of a flying-boat hull of high length-beam ratio

A mathematical theory of plasticity based on the concept of slip

Response of a helicopter rotor to oscillatory pitch and throttle movements

Investigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wings

Gust-tunnel investigation of a wing model with semichord line swept back 30 degrees

The effects of aerodynamic brakes upon the speed characteristics of airplanes

Direct-reading design charts for 24S-T aluminum-alloy flat compression panels having longitudinal straight-web Y-section stiffeners

Theoretical analysis of oscillations of a towed cable

A study of stall phenomena on a 45 degree swept-forward wing

Overbalancing in residual-liquidation computations

Comparison of over-all impact loads obtained during seaplane landing tests with loads predicted by hydrodynamic theory

Flow studies in the asymmetric adjustable nozzle of the Ames 6-by 6-foot supersonic wind tunnel

Investigation of internal regenerative fuel-heating system for 20-inch ram jet

Investigation of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel IV : the effect of a constant-chord leading-edge flap at high subsonic speeds

Investigation of extensible wing-tip ailerons on an untapered semispan wing at 0 degree and 45 degrees sweepback

Investigation of a thin wing of aspect ratio 4 in the Ames 12-foot pressure wind tunnel V : static longitudinal stability and control throughout the subsonic speed range of a semispan model of a supersonic airplane

The effects of scale and test technique on the validity of small-scale measurements of the aerodynamic characteristics of a wing with the leading edge swept back 63 degrees

Investigation of a thin straight wing of aspect ratio 4 by the NACA wing-flow method: Lift and pitching-moment characteristics of the wing alone

Investigations of an annular diffuser-fan combination handling rotating flow

Investigation of several clamshell variable-area exhaust nozzles for turbojet engines

Method of determining centrifugal-flow-compressor performance with water injection

Wing-tunnel investigation at low transonic speeds of the effects of number of wings on the lateral-control effectiveness of an RM-5 test vehicle

Analysis of measured pressures on airfoils at Mach numbers near 1

A preliminary experimental investigation of a submerged cascade inlet

Preliminary experimental investigation of effects of aerodynamic shape of concentrated weights on flutter of a straight cantilever wing

Preliminary investigation of a variable mass-flow supersonic nose inlet

Wind-tunnel investigation of transonic aileron flutter

Preliminary full-scale investigation of a 1/3-scale model of a convertible-type airplane

Pressure-distribution data for the NACA 64(sub 1)-012 and 64(sub 1) A012 airfoils at high subsonic Mach numbers

Preliminary Wind-Tunnel Tests of Triangular and Rectangular Wings in Steady Roll at Mach Numbers of 1.62 and 1.92

Lateral and directional stability and control characteristics of a C-54D airplane

Determination of rate, area, and distribution of impingement of water drops on various airfoils from trajectories obtained on the differential analyzer

Vibrational modes of several hollow turbine blades and of solid turbine blade of similar aerodynamic design

Downwash in vortex region behind trapezoidal-wing tip at Mach number 1.91

Analytical determination of effect of water injection on power output of turbine-propeller engine

Aerodynamic characteristics of a wing with quarter-chord line swept back 35 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section : transonic-bumb method

Carbon deposition from AN-F-58 fuels in a J33 single combustor

Comparison of effectiveness of coordinated turns and level sideslips for correcting lateral displacement during landing approaches

Aerodynamic characteristics of a wing with quarter-chord line swept back 60 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section: transonic-bump method

Aerodynamic characteristics of a wing with unswept quarter-chord line, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section

The aerodynamic characteristics throughout the subsonic speed range of a thin, sharp-edged horizontal tail of aspect ratio 4 equipped with a constant-chord elevator

Analysis and experimental observation of pressure losses in ram-jet combustion chambers

An analysis of a highly compounded two-stroke-cycle compression-ignition engine

Evaluation of piston-type gas-generator engine for subsonic transport operation.

Effects of Mach number and sweep on the damping-in-roll characteristics of wings of aspect ratio 4

Effects of systematic changes of trailing-edge angle and leading-edge radius on the variation with Mach number of the aerodynamic characteristics of a 10-percent-chord-thick NACA airfoil section

Estimated transonic flying qualities of a tailless airplane based on a model investigation

Estimation of the forces and moments acting on inclined bodies of revolution of high fineness ratio


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