Browse TRAIL Inventories

Investigation at low speed of the downwash, sidewash, and wake characteristics behind a large-scale triangular wing, including the effects of yaw, full-span trailing-edge flaps, and two leading-edge modifications

Investigation at high subsonic speeds of bodies mounted from the wing of an unswept-wing-fuselage model, including measurements of body loads

Effect of free methyl radicals on slow oxidation of propane and ethane

Distribution of fissionable material in thermal reactors of spherical geometry for uniform power generation

Effect of camber and twist on the stability characteristics of models having a 45 degree swept wing as determined by the free-fall method at transonic speeds

Facilities and methods used in full-scale airplane crash-fire investigation

Cooling characteristics of an experimental tail-pipe burner with an annular cooling-air passage

Experimental investigation of the stability, control, and induced rolling moments of a canard missile airframe at a Mach number of 1.7

Experimental investigation of the static aerodynamic and dynamic damping-in-roll characteristics of an 8-cm aircraft rocket with solid and slotted fins

An experimental investigation of the zero-lift pressure distribution over a wedge airfoil in closed, slotted, and open-throat tunnels at transonic Mach numbers

Dynamic corrosion of a stainless-steel specimen by water at 500 F using a toroid circulating apparatus /c Leland G. Desmon, Don R. Mosher

Free-flight investigation of longitudinal stability and control of a rocket-propelled missile model having cruciform, triangular, inline wings and tails

Chordwise pressure distribution at high subsonic speeds near midsemispan of a tapered 35 degree sweptback wing of aspect ratio 4 having NACA 65A006 airfoil sections and equipped with various spoiler ailerons

Investigation of the hydrodynamic stability and resistance of two streamline fuselages

The effects on the aerodynamic characteristics of varying the wing thickness ratio of a triangular wing-body configuration at transonic speeds from tests by the NACA wing-flow method

Effects of simulated skin wrinkles on the wing surface on the aerodynamic characteristics of two wing-body combinations employing wings of low aspect ratio at subsonic and supersonic speeds

Lift, drag and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds: Plane tapered wing of aspect ratio 3.1 with 3-percent-thick rounded-nose section

Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds: Twisted and cambered triangular wing of aspect ratio 2 with NACA 0005-63 thickness distribution

Low-speed longitudinal aerodynamic characteristics of a twisted and cambered wing of 45 degree sweepback and aspect ratio 8 with and without high-lift and stall-control devices and a fuselage at Reynolds numbers from 1.5 x 10(exp 6) to 4.8 x 10(exp 6

Studies of the flow field behind a large scale 47.5 degree sweptback wing having circular-arc airfoil sections and equipped with drooped-nose and plain flaps

A unified two-dimensional approach to the calculation of three-dimensional hypersonic flows, with application to bodies of revolution

Effect of vertical location of a horizontal tail on the static longitudinal stability characteristics of a 45 degree sweptback-wing-fuselage combination of aspect ratio 8 at a Reynolds number of 4.0 x 10(exp 6)

Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen biflouride as oxidant for rocket engines 1: mixture of liquid ammonia and hydrazine

Some effects of side-wall modifications on the drag and pressure recovery of an NACA submerged inlet at transonic speeds

Low-speed aerodynamic characteristics of a large-scale 60 degree swept-back wing with high lift devices

Pressure distribution and pressure drag for a hemispherical nose at Mach numbers 2.05, 2.54, and 3.04

Internal-film-cooling experiments with 2- and 4-inch smooth-surface tubes and gas temperatures to 2000 degrees Fahrenheit

Flight calibration of angle-of-attack and sideslip detectors on the fuselage of a 35 degree swept-wing fighter airplane

Small-scale transonic investigation of the effects of twist and camber on the aerodynamic characteristics of a 60 degrees 42' sweptback wing of aspect ratio 1.94

Free-flight measurements of some effects of aileron span, chord, and deflection and of wing flexibility on the rolling effectiveness of ailerons on sweptback wings at Mach numbers between 0.8 and 1.6

Summary of some effective aerodynamic twisting-moment coefficients of various wing-control configurations at Mach numbers from 0.6 to 1.7 as determined from rocket-powered models

A pressure-distribution investigation of a fineness-ratio-12.2 parabolic body of revolution (NACA RM-10) at M = 1.59 and angles of attack up to 36 degrees

Reciprocity relations in aerodynamics

Simple Graphical Solution of Heat Transfer and Evaporation From Surface Heated to Prevent Icing

A Probability Analysis of the Meteorological Factors Conducive to Aircraft Icing in the United States

Experimental Investigation of Boundary-Layer Suction Through Slots to Obtain Extensive Laminar Boundary Layers on a 15 Percent-Thick Airfoil Section at High Reynolds Numbers

Supplementary Free-Spinning-Tunnel Investigation of a 1/20-Scale Model of the McDonnell F2H-3 Airplane With External Stores Installed

Development of a Laminar Boundary Layer Behind a Suction Point

Boundary-Layer Measurements on Several Porous Materials With Suction Applied

Experimental Investigation of an NACA 64A010 Airfoil Section With 41 Suction Slots on Each Surface for Control of Laminar Boundary Layer

On the Design of Airfoils in Which the Transition of the Boundary Layer Is Delayed

Experimental Study of the Effects of Finite Surface Disturbances and Angle of Attack on the Laminar Boundary Layer of an NACA 64A010 Airfoil With Area Suction

Experimental Investigation of the Stability, Control, and Induced Rolling Moments of a Canard Missile Airframe at a Mach Number of 1.7

Comparison of Three Multicylinder Icing Meters and Critique of Multicylinder Method

A Study of Poisson's Ratio in the Yield Region

Two-Dimensional Steady Nonviscous and Viscous Compressible Flow Through a System of Equidistant Blades

A Miniature Electrical Pressure Gage Utilizing a Stretched Flat Diagram

An Approach to the Prediction of the Frequency Distribution of Gust Loads on Airplanes in Normal Operations

Investigation of the Structural Damping of a Full-Scale Airplane Wing

Fatigue Strengths of 14S-T4 Aluminum Alloy Subjected to Biaxial Tensile Stresses


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