Browse TRAIL Inventories

Two-dimensional cascade tests of NACA 65-(C(sub zeta)(sub o))A(sub 10))10 blade sections at typical compressor hub conditions for speeds up to choking

Preliminary investigation of dynamic lateral stability characteristics of a configuration of the North American X-15 research airplane

Theoretical performance of liquid hydrogen and liquid fluorine as a rocket propellant for a chamber pressure of 600 pounds per square inch absolute

A summary of the longitudinal and lateral stability and control characteristics obtained from rocket-model tests of a swept-wing fighter-type airplane at Mach numbers from 0.5 to 1.9

Theoretical rocket performance of JP-4 fuel with mixtures of liquid ozone and fluorine

Temperature measurements from a flight test of two wing-body combinations at 7 degree angle of attack for Mach numbers to 4.86 and Reynolds numbers to 19.2 X 10(exp 6)

Investigation of the planing lift of a flat plate at speeds up to 170 feet per second

Effect of bluntness on transition for a cone and a hollow cylinder at Mach 3.1

Free-flight investigation of jet effect on the low-lift drag and longitudinal trim of a supersonic interceptor-type airplane configuration with an overhanging tail boom at Mach numbers from 1.09 to 1.34

Experimental investigation of the forces and moments due to sideslip of a series of triangular vertical- and horizontal-tail combinations at Mach numbers of 1.62, 1.93, and 2.41

Propellant vaporization as a criterion for rocket-engine design : experimental effect of fuel temperature on liquid-oxygen - heptane performance

A study of injection processes for 15-percent fluorine - 85-percent oxygen and heptane in a 200-pound-thrust rocket engine

Aerodynamic heating of a thin, unswept, untapered, multiweb, aluminum-alloy wing at Mach numbers up to 2.67 as determined from a free-flight investigation of a rocket-propelled model

Performance of an experimental annular turbojet combustor with methane and propane

Vertical force-deflection characteristics of a pair of 56-inch-diameter aircraft tires from static and drop tests with and without prerotation

Investigation of the effects of propeller diameter on the ability of a flapped wing, with and without boundary-layer control, to deflect a propeller slipstream downward for vertical take-off

High altitude performance investigation of J65-B-3 turbojet engine with both JP-4 and gaseous hydrogen fuels

Interference effects of fuselage-stored missiles on inlet duct model of an interceptor-type aircraft at Mach numbers 1.5 to 1.9

Experimental investigation of effects of simulated nacelles and wing-root freedoms on supersonic flutter characteristics of a cambered, modified, swept, tapered wing

Design and performance of flight-type liquid-hydrogen heat exchanger

Experimental Investigation of Effects of Combustion-chamber Length and Inlet Total Temperature, Total Pressure, and Velocity on Afterburner Performance

Altitude free-jet investigation of dynamics of a 28-inch-diameter ram-jet engine

Altitude chamber evaluation of an aircraft liquid hydrogen fuel system used with a turbojet engine

Reaction of fluorine with carbon as a means of fluorine disposal

Investigation of Heat Transfer from a Stationary and Rotating Conical Forebody

Experimental Droplet Impingement on Four Bodies of Revolution

Free-Flight Skin Temperature and Pressure Measurements on a Slightly Blunted 25 Deg Cone-Cylinder-Flare Configuration to a Mach Number of 9.89

Statistical Study of Aircraft Icing Probabilities at the 700- and 500- Millibar Levels over Ocean Areas in the Northern Hemisphere

Effects of Some Configuration Changes on Afterburner Combustion Performance

Boundary-Layer-Transition and Heat-Transfer Measurements from Flight Tests of Blunt and Sharp 50 Degree Cones at Mach Numbers from 1.7 to 4.7

An Investigation at Low Speed of the Spin Instability of Mortar-Shell Tails

A Study of Injection Processes for 15-percent Fluorine-85- Percent Oxygen and Heptane in a 200-pound-thrust Rocket Engine

Experimental investigation of effects of moderate sideslip on the flow fields near a 45 degree swept-wing-fuselage combination at low speed

Summary of scale-model thrust-reverser investigation

Relation of Turbojet and Ramjet Combustion Efficiency to Second-Order Reaction Kinetics and Fundamental Flame Speed

Heat of Combustion of the Product Formed by the Reaction of Acetylene and Diborane (LFPL-CZ-3)

Comparison of the Combustion Performance of Shell UMF, Grade C, MIL-F-5624C, Grade JP-5, Fuels in a Heavy-Duty XRJ47-W-9 Ram-Jet Engine

Endurance Evaluation of Sintered, Porous, Strut-Supported Turbine Blades made by Federal-Mogul-Bower-Bearings, Incorporated, under Bureau of Aeronautics Contract NOas 55-124-C

Two-dimensional airfoil characteristics of four NACA 6A-series airfoils at transonic Mach numbers up to 1.25

Minimum wave drag for arbitrary arrangements of wings and bodies

Seat Design for Crash Worthiness

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-wing airplane

On flow of electrically conducting fluids over a flat plate in the presence of a transverse magnetic field

Some effects of bluntness on boundary-layer transition and heat transfer at supersonic speeds

Three-dimensional transonic flow theory applied to slender wings and bodies

Flight investigation of the effectiveness of an automatic aileron trim control device for personal airplanes

A variational theorem for creep with applications to plates and columns

On panel flutter and divergence of infinitely long unstiffened and ring-stiffened thin-walled circular cylinders

Extended operation of turbojet engine with pentaborane

Cloud-droplet ingestion in engine inlets with inlet velocity ratios of 1.0 and 0.7


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