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Effects of wing inboard plan-form modifications on lift, drag, and longitudinal stability at Mach numbers from 1.0 to 2.3 of a rocket-propelled free-flight model with a 52.5 degree sweptback wing of aspect ratio 3

Wind-tunnel investigation of the effect of aspect ratio and chordwise location on effectiveness of spoiler-slot-deflector controls on thin untapered winds at transonic speeds

Flight investigation of a ram jet burning magnesium slurry fuel and having a conical shock inlet designed for a Mach number of 4.1

Investigation of transonic flutter characteristics of a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6

Flutter at very high speeds

Effects on adjacent surfaces from the firing of rocket jets

Span loadings due to wing twist at transonic and supersonic speeds

Investigation at Mach numbers from 0.80 to 1.43 of pressure and load distributions over a thin 45©� sweptback highly tapered wing in combination with basic and indented bodies

Aerodynamic characteristics of a spoiler-slot-deflector control on a 45©� sweptback wing at Mach numbers of 1.61 and 2.01

Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers

Investigation of the aerodynamic characteristics in pitch and sideslip of a 45©� swept-wing airplane configuration with various vertical locations of the wing and horizontal tail.Static lateral and directional stability; Mach numbers of 1.41 and 2.01

Theoretical rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming frozen composition

Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet

Flight measurements of airplane structural temperatures at supersonic speeds

Stability of two rocket-propelled models having aspect-ratio-5 unswept tails on a long body for the Mach number range of 1.7 to 2.4

Summary of 65-Series Compressor-Blade Low-Speed Cascade Data by Use of the Carpet-Plotting Technique

Experimental Investigation of Vibratory Stresses in a Concentric-Ring Direct-Air-Cycle Nuclear Fuel Element

Aerodynamic Characteristics of a 0.04956-Scale Model of the Convair TF-102A Airplane at Transonic Speeds, Coord. No. AF-120

Preliminary Internal Performance Data for a Variable-Ejector Assembly on the XJ79-GE-1 Turbojet Engine, II, Afterburning Configurations

Turbulence in the Wake of a Thin Airfoil at Low Speeds

Blow-Out Velocities of Solutions of Hydrocarbons and Boron Hydride - Hydrocarbon Reaction Products in a 1 7/8-Inch-Diameter Combustor

A Fuselage Addition to Delay Drag-Rise Mach Number of Subsonic Airplanes at Lifting Conditions

Surge-Inception Study in a Two-Spool Turbojet Engine, Revised

Free-flight investigation at transonic speeds of the power-on characteristics including some effects of sonic propulsive jets of a four-engine delta-wing configuration

Free-flight investigation of comparative zero-lift rolling effectiveness of a leading edge and a trailing edge air-jet spoiler on an unswept wing

Tensile properties of Inconel X sheet under rapid-heating and constant-temperature conditions

Tensile stress-strain properties of 17-7 PH and AM 350 stainless-steel sheet at elevated temperatures

Chemical igniters for starting jet fuel - nitric acid rockets

A simplified method for assessing the effect of steady rolling on angle of attack and sideslip

A theoretical and experimental study of planing surfaces including effects of cross section and plan form

On possible similarity solutions for three-dimensional incompressible laminar boundary layers 3: similarity with respect to stationary polar coordinates for small angle variation

An investigation at low speed of the flow over a simulated flat plate at small angles of attack using pitot-static and hot-wire probes

A correlation of low-speed, airfoil-section stalling characteristics with Reynolds number and airfoil geometry

Cascade investigation of a related series of 6-percent-thick guide-vane profiles and design charts

Basic performance characteristics of several subsonic-diffuser-bypass-duct combinations for use with supersonic inlets

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


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