TRAIL - Technical Report Archive and Image Library

Lift, drag, and pitching moment of low-aspect-ratio wings at subsonic and supersonic speeds : an investigation at large Reynolds numbers of the low-speed characteristics of several wing-body combinations

Effects on the weight-flow range and efficiency of a typical axial-flow compressor inlet stage that result from the use of a decreased blade camber or decreased guide-vane turning

Pressure drop in coolant passages of two air-cooled turbine-blade configurations

Transonic free-flight investigation of the total drag and of the component drags (cowl pressure, additive, base, friction, and internal) encountered by a 16-inch-diameter ram-jet engine for Mach numbers from 0.80 to 1.43

Performance of supersonic scoop inlets

Investigation at high and low subsonic Mach numbers of two symmetrical 6-percent-thick airfoil sections designed to have high maximum lift coefficients at low speeds

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

Ignition delay experiments with small-scale rocket engine at simulated altitude conditions using various fuels with nitric acid oxidants / Dezso J. Ladanyi

Free-spinning-tunnel investigation of a 1/30-scale model of the Grumman XS2F-1 airplane: TED No. NACA DE 366

Friction and surface damage of several corrosion-resistant materials

Effect of design changes and operating conditions on combustion and operational performance of a 28-inch diameter Ram-jet engine / T. B. Shillito and Shigeo Nakanishi

Free-flight tests at Mach numbers from 0.8 to 1.4 to determine the effect on zero-lift drag of increasing the leading-edge bluntness of a 45 degree sweptback wing having an NACA 65A009 airfoil

Measurements of thermal distortion of the submarine intermediate reactor "Mark A" moderator tube

Effect of current design trends on airplane spins and recoveries

Effect of fuel density and heating value on ram-jet airplane range

Correlation of buffet boundaries predicted from wind-tunnel tests with those measured during flight tests on the F8F-1 and X-1 airplanes -transonic-bump method

A Correlation by Means of the Transonic Similarity Rules of the Experimentally Determined Characteristics of 22 Rectangular Wings of Symmetrical Profile

Correlation of predicted and experimental lateral oscillation characteristics for several airplanes

Design and test of mixed-flow impellers 2: experimental results, impeller model MFI-1A

Design and test of mixed-flow impellers 1: aerodynamic design procedure

Design of apparatus for determining heat transfer and frictional pressure drop of nitric acid flowing through a heated tube

Effect of magnitude of vibratory load superimposed on mean tensile load on mechanism of and time to fracture of specimens and correlation to engine blade

Effect of oxygen concentration of the inlet oxygen-nitrogen mixture on the combustion efficiency of a single J33 turbojet combustor

Aerodynamic characteristics of two 25-percent-area trailing-edge flaps on an aspect ratio 2 triangular wing at subsonic and supersonic speeds

An analytical method for evaluating factors affecting application of transpiration cooling to gas turbine blades

An analytical study of the comparative performance of four air-induction systems for turbojet-powered airplanes designed to operate at Mach numbers up to 1.5

Analytical study of static and low-speed performance of thin propellers using two-speed gear ratios to obtain optimum rotational speeds

Comparison of calculated and experimental temperatures of water-cooled turbine blades

Combustion efficiency of homogeneous fuel-air mixtures in a 5-inch ram-jet-type combustor

Analysis of stage matching and off-design performance of multistage axial-flow compressors

The aerodynamic characteristics of a supersonic aircraft configuration with a 40 degree sweptback wing through a Mach number range from 0 to 2.4 obtained from various sources

Aerodynamic characteristics of two-plane, unswept tapered wings of aspect ratio 3 and 3-percent thickness from tests on a transonic bump

Characteristics of flap-type spoiler ailerons at various locations on a 60 degree delta wing with a double slotted flap

Characteristics of swept wings at high speeds

Combustion efficiency performance of a MIL-F-5624 type fuel and monomethylnapthalene in a single vaporizing combustor

Component and over-all performance evaluation of an axial-flow turbojet engine over a range of engine-inlet Reynolds numbers

Analysis of coolant-flow requirements for an improved, internal-strut-supported, air-cooled turbine-rotor blade

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