Browse TRAIL Inventories

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

Proposed initiating system for crash-fire prevention systems

Relation of turbojet propulsion system development to the strategic bomber mission

Summary of Scale-model thrust-reverser investigation

Section characteristics of the NACA 0006 airfoil with leading-edge and trailing-edge flaps

Study of ram-air heat exchangers for reducing turbine cooling-air temperature of a supersonic aircraft turbojet engine

A study of several factors affecting the stability contributed by a horizontal tail at various vertical positions on a sweptback-wing airplane model

Study of size effect in sheet-stringer panels

A horizontal-tail arrangement for counteracting static longitudinal instability of sweptback wings

Lift and pitching-moment interference between a pointed cylindrical body and triangular wings of various aspect ratios at Mach numbers of 1.50 and 2.02

Ignition delays and fluid properties of several fuels and nitric acid oxidants in temperature range from 70 to -105 degrees Fahrenheit

Flight investigation of the effect of vertical-tail size on the rolling behavior of a swept-wing airplane having lateral-longitudinal coupling

Investigation at supersonic speeds of the effects of bomb-bay configuration upon the aerodynamic characteristics of fuselages with noncircular cross sections

Investigation by the transonic-bump method of a 35 degree sweptback semispan model equipped with a flap operated by a series of servovanes located ahead of and geared to the flap

An investigation at subsonic speeds of several modifications to the leading-edge region of the NACA 64A010 airfoil section designed to increase maximum lift

Investigation at zero forward speed of a leading-edge slat as a longitudinal control device for vertically rising airplanes that utilize the redirected-slipstream principle

An investigation at Mach numbers of 1.41 and 2.01 of the aerodynamic characteristics of a swept-wing supersonic bomber configuration

Theoretical calculation of the power spectra of the rolling and yawing moments on a wing in random turbulence

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

Transonic wind-tunnel investigation of the effects of indentation on the wing loads of a 45 degree sweptback wing-body combination

Transonic wind-tunnel measurements of static lateral and directional stability and vertical-tail loads for a model with a 45 degree sweptback wing

Tank investigation of a series of related hydro-skis as load-alleviation devices for landing a seaplane in waves

Summary of derived gust velocities obtained from measurements within thunderstorms

Tank tests of a 1/8-size powered dynamic model of the Martin PBM-5 seaplane equipped with a single Edo hydro-ski : TED No. NACA AD3110

Thermal decomposition of ethylpentaborane in gas phase

Aerodynamic principles for the design of jet-engine induction systems

Aerodynamic loadings associated with swept and unswept spoilers on a flat-plate at Mach numbers of 1.61 and 2.01

A theoretical study of the lifting efficiency at supersonic speeds of wings utilizing indirect lift induced by vertical surfaces

Theoretical pressure distributions for some slender wing-body combinations at zero lift

Wind-tunnel investigation of jet-augmented flaps on a rectangular wing to high momentum coefficients

Altitude performance of J71-A-2(600-D1) turbojet engine

Altitude performance evaluation of J71-A-11 turbojet engine

Turbulent shear spectra and local isotropy in the low-speed boundary layer

Aerodynamic and hydrodynamic characteristics of a deck-inlet multijet water-based-aircraft configuration designed for supersonic flight

Additional results of an investigation at transonic speeds to determine the effects of a heated propulsive jet on the drag characteristics of a series of related afterbodies

Theoretical wave drag of shrouded airfoils and bodies


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