Browse TRAIL Inventories

General tank tests on the hydrodynamic characteristics of four flying-boat hull models of differing length-beam ratio

General resistance tests on flying-boat hull models

An investigation of aircraft heaters XVI : determination of the viscosity of exhaust gases from a gasoline engine

Use of Internal Coolant as a Means of Permitting Increase in Engine Take-Off Power

Wind tunnel investigation of NACA 66(215)-216, 66,1-212, and 65(sub 1)-212 airfoils with 0.20-airfoil-chord split flaps

Tests of the Northrop MX-334 glider airplane in the NACA full-scale tunnel

A positive-replica technique for examining finished metal surfaces and its application to aircraft engine cylinders

Preknock vibrations in a spark-ignition engine cylinder as revealed by high-speed photography

Charts for calculation of the critical compressive stress for local instability of idealized web- and T-stiffened panels

Engine and inspection tests of methyl tert-butyl ether as a component of aviation fuel

End-zone water injection as a means of suppressing knock in a spark-ignition engine

Fatigue tests of riveted joints : progress report of tests of 17S-T and 53S-T joints

Accelerations and bottom pressures measured on a B-24D airplane in a ditching test

The knock-limiting performance of fuel blends containing aromatics Part 1: toluene, ethyl-benzene, and p-xylene

Knock-limited performance of pure hydrocarbons blended with a base fuel in a full-scale aircraft-engine cylinder 2: twelve aromatics

The knock-limited performance of several miscellaneous fuels blended with a base fuel I

Knock-limited performance of blends of AN-F-28 fuel containing 2 percent aromatic amines 1

Knock-limited performance of blends of AN-F-28 fuel containing 2 percent aromatic amines II

Knock-limited performance of blends of AN-F-28 fuel containing 2 percent aromatic amines III

Wind Tunnel Investigation of the Effect of Jet-Motor Operation Stability

Flight measurements of horizontal tail loads on a typical propeller-driven pursuit airplane during stalled pull-outs at high speed

Effect of several methods of increasing knock-limited power on cylinder temperatures

Analysis and correlation of data obtained by six laboratories on fuel-vapor loss from fuel tanks during simulated flight

Application of the method of least squares to engine-cooling analysis

Breaking aircraft-engine oil foams by use of electrically charged condenser plates

Wind-tunnel procedure for determination of critical stability and control characteristics of airplanes

Spin-tunnel tests of a 1/57.33-scale model of the Northrop XB-35 airplane

Wall interference in a two-dimensional-flow wind tunnel, with consideration of the effect of compressibility

Climb and high-speed tests of a Curtiss number 714-1C2-12 four-blade propeller on the Republic P-47C airplane

On the Flow of a Compressible Fluid by the Hodograph Method. II - Fundamental Set of Particular Flow Solutions of the Chaplygin Differential Equation

Wind Tunnel Investigation of the Effects of Slot Shape and Flap Location on the Characteristics of a Low-Drag Airfoil Equipped with a 0.25-Chord Slotted Flap

Wind-tunnel investigation of ailerons on a low-drag airfoil 1: The effect of aileron profile

Wind-tunnel investigation of the effects of profile modification and tabs on the characteristics of ailerons on a low-drag airfoil

Wind-tunnel investigation of ailerons on a low-drag airfoil 2: the effect of thickened and beveled trailing edges

Full-scale wind-tunnel investigation of forward underslung cooling-air ducts

High-speed aerodynamic characteristics of a four-engine bomber airplane as determined from tests of a 0.075-scale model

High-altitude cooling VI : axial-flow fans and cooling power

High-altitude cooling IV : intercoolers

High-altitude cooling II : air-cooled engines

High-altitude cooling V : cowling and ducting

High-altitude cooling I : resume of the cooling problem

High-speed aerodynamic characteristics of a four-engine transport airplane as determined from tests of a 0.075-scale model

An investigation of aircraft heaters 17: experimental inquiry into steady state unidirectional heat-meter corrections

Intercooler cooling-air weight flow and pressure drop for minimum drag loss

An investigation of aircraft heaters 15: the emissivity of several materials

An investigation of aircraft heaters 14: an air and heat flow analysis of a ram-operated heater and duct system

An investigation of aircraft heaters 24: the heat meter in the transient state for unidirectional heat transfer

An interim report on the stability and control of tailless airplanes

A method for welding sheet aluminum to SAE 4140 steel

A method for the rapid estimation of turbulent boundary-layer thickness for calculating profile drag


Published Year

Subject

Author

‹‹ previous 1 2 ... 18 19 20 21 22 23 24 ... 83 84 next ››