TRAIL - Technical Report Archive and Image Library

Component tests to determine the aerodynamic characteristics of an all-moveable 70 degree delta canard-type control in the presence of a body at a Mach number of 1.61

Comparison of measured and predicted indicated angles of attack near the fuselages of a triangular-wing wind-tunnel model and a swept-wing fighter airplane in flight

A transonic wind-tunnel investigation of the effects of body indentation, as specified by the transonic drag-rise rule, on the aerodynamic characteristics and flow phenomena of an unswept-wing-body combination

Characteristics of a canard-type missile configuration with an underslung scoop inlet at Mach numbers from 1.5 to 2.0

Effect of variations in Reynolds number on the aerodynamic characteristics of three bomb or store shapes at a Mach number of 1.62 with and without fins

Evaporation and spreading of isooctane sprays in high velocity air streams

The effects of leading-edge extensions, a trailing-edge extension, and a fence on the static longitudinal stability of a wing-fuselage-tail combination having a wing with 35 degrees of sweepback and an aspect ratio of 4.5

Effective thermal conductivities of magnesium oxide stainless steel, and uranium oxide powders

The effects of nacelles and of extended split flaps on the longitudinal characteristics of a wing-fuselage-tail combination having a wing with 40 degrees of sweepback and an aspect ratio of 10

Estimation of water landing loads on hydro-ski-equipped aircraft

Effects of trailing-edge bluntness on the lift, drag, and pitching-moment characteristics of unswept, 45 degree swept, and 45 degree delta wings at Mach numbers of 1.41, 1.62, and 1.96

Experimental investigation of laminar-boundary-layer control on an airfoil section equipped with suction slots located at discontinuities in the surface pressure distribution

Experimental investigation of physical and combustion properties of several residual fuel oils and magnesium - fuel-oil slurries in a ram-jet-type combustor

Experimental investigation of screeching combustion in full-scale afterburner

Experimental investigation of several water-injection configurations for turbine-blade spray cooling in a turbojet engine

Experimental and theoretical study of the interference at low speed between slender bodies and triangular wings

Experimental investigation of the effect of entrance width-to-height ratio on the performance of an auxiliary scoop-type inlet at Mach numbers from 0 to 1.3

An experimental investigation of the effect of various parameters including tip Mach number on the flutter of some model helicopter rotor blades

Experimental investigation of the effects of plan-form taper on the aerodynamic characteristics of symmetrical unswept wings of varying aspect ratio

Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a Mach number of 2.01

Aerodynamic characteristics of a 68.4 degree delta wing at Mach numbers of 1.6 and 1.9 over a wide Reynolds number range

The aerodynamic characteristics at transonic speeds of an all-movable, tapered, 45 degree sweptback, aspect-ratio-4 tail deflected about a skewed hinge axis and equipped with an inset unbalancing tab

Aluminum borohydride as an ignition source for turbojet combustors

Tests in the Ames 40- by 80-foot wind tunnel of an airplane model with an aspect ratio 4 triangular wing and an all-movable horizontal tail - high-lift devices and lateral controls

Results of a rocket-model investigation of control-surface buzz and flutter on a 4-percent-thick unswept wing and on 6-, 9-, and 12-percent-thick swept wings at transonic speeds

Results of measurements of maximum lift and buffeting intensities obtained during flight investigation of the Northrop X-4 research airplane

Some fundamental aspects of nitric acid oxidants for rocket applications

Some observations on stall flutter and buffeting

Slotted-boundary interference effects on wedge airfoils at low supersonic Mach numbers

Some torsional-damping measurements of laminated beams as applied to the propeller stall-flutter problem

Static aeroelastic phenomena of M-, W-, and A-wings

Static crucible investigation of corrosion and mass-transfer of nickel in molten sodium hydroxide with various additives

Summary of pitch-damping derivatives of complete airplane and missile configurations as measured in flight at transonic and supersonic speeds

Tests in the Ames 40- by 80-foot wind tunnel of two airplane models having aspect ratio 2 trapezoidal wings of taper ratios 0.33 and 0.20

Experimental investigation of aerodynamically balanced trailing-edge control surfaces on an aspect ratio 2 triangular wing at subsonic and supersonic speeds

An experimental study of porosity characteristics of perforated materials in normal and parallel flow

The effect at high subsonic speeds of a flap-type aileron on the chordwise pressure distribution near midsemispan of a tapered 35 degree sweptback wing of aspect ratio 4 having NACA 65A006 airfoil section

The effects of extensible rocket racks on lift, drag, and stability of a 1/10-scale rocket-boosted model of the McDonnell XF3H-1 airplane for a Mach number range of 0.60 to 1.34 : TED No. NACA DE 31

Effects of high degrees of biaxial stretch forming on crazing and other properties of acrylic plastic glazing

Effects of nitrogen tetroxide and water concentration on freezing point and ignition delay of fuming nitric acid

Comparison of ignition delays of several propellant combinations obtained with modified open-cup and small-scale rocket engine apparatus

Ignition delays of alkyl thiophosphites with white and red fuming nitric acids within temperature range 80 to -105 degrees Fahrenheit

A flight investigation of the effect of leading-edge camber on the aerodynamic characteristics of a swept-wing airplane

Investigation of 16-inch impulse-type supersonic compressor rotor with turning past axial direction

Investigation at transonic speeds of aerodynamic characteristics of a semielliptical air inlet in the root of a 45 degree sweptback wing

A theory for stability and buzz pulsation amplitude in ram jets and an experimental investigation including scale effects

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