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

Preliminary report on a study of separated flows in supersonic and subsonic streams

Some effects of guide-vane turning and stators on the rotating stall characteristics of a high hub-tip ratio single-stage compressor

Some effects of small-scale flow disturbance on nozzle-burner flames

Thermodynamic study of air-cycle and mercury-vapor-cycle systems for refrigerating cooling air for turbines or other components

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

Thermodynamic properties of products of combustion of hydrogen with air fo r temperatures of 600 to 4400 R

Analytic evaluation of effect of inlet-air temperature and combustion pressure on combustion performance of boron slurries and blends of pentaborane in octene-1 : supplement I- influence of new boric-oxide vapor-pressure data on calculated performanc

Analysis of turbomachine viscous losses affected by changes in blade geometry

Analysis of turbojet-engine controls for afterburning starting

Analysis of the vertical-tail loads measured during a flight investigation of the Douglas X-3 research airplane

The appearance of a boric oxide exhaust cloud from a turbojet engine operating on trimethylborate fuel

Wind-tunnel investigation of the effect of aspect ratio and chordwise location on effectiveness of plain spoilers on thin untapered wings at transonic speeds

Wind-tunnel investigation of the effect of clipping the tips of triangular wings of different thickness, camber, and aspect ratio - transonic bump method

Wind-tunnel investigation of the aerodynamic characteristics in pitch of wing-fuselage combinations at high subsonic speeds: taper-ratio series

Theoretical lift due to wing incidence of slender wing-body-tail combinations at zero angle of attack

Visualization of rotor tip secondary flows with blade tip air discharge and suction in a low-speed turbine

Wind-tunnel investigation of two vertical-takeoff-and-landing jet bomber airplane configurations at Mach numbers of 1.94 and 2.40

Wind-tunnel investigation to determine the horizontal- and vertical-tail contributions to the static lateral stability characteristics of a complete-model swept-wing configuration at high subsonic speeds

Experimental investigation at high subsonic speed of the rolling stability derivatives of a complete model having a clipped-delta wing and a high horizontal tail

An experimental investigation at Mach numbers from 2.1 to 3.0 of circular-internal-contraction inlets with translating centerbodies

Flight investigation of the stability and control characteristics of vertically rising airplane research model with swept or unswept wings and x- or +-tails

Experimental investigation of a high subsonic Mach number turbine having high rotor blade suction-surface diffusion

Experimental investigation of air-flow uniformity and pressure level on wire cloth for transpiration-cooling applications

Experimental investigation of air-side performance of liquid-metal to air heat exhangers

Experimental investigation of a high subsonic Mach number turbine having low rotor suction-surface diffusion

Experimental investigation of a transonic compressor rotor with a 1.5-inch chord length and an aspect ratio of 3.0 III : blade-element and over-all performance at three solidity levels

Free-flight tests of 1/10-scale Republic F-105 airplane wings in the subsonic to low supersonic speed range to investigate the possibility of flutter : COORD. No. AF-224

Flight measurements of horizontal-tail loads on the Douglas X-3 research airplane

Static strength of aluminum-alloy specimens containing fatigue cracks

An evaluation of four experimental methods for measuring mean properties of a supersonic turbulent boundary layer

Effect of several design variables on internal performance of convergent-plug exhaust nozzles

An investigation of the lift, drag, and static-stability characteristics of a triangular-wing airplane configuration at Mach numbers from 3.00 to 6.28

An investigation of the loads on the vertical tail of a jet-bomber airplane resulting from flight through rough air

Investigation of boundary-layer transition on 10 degree cone in langley 4- by 4-foot supersonic pressure tunnel at Mach numbers of 1.41, 1.61, and 2.01

Coking of JP-4 fuels in electrically heated metal tubes

Effects of compressor interstage bleed and adjustable inlet guide vanes on compressor stall characteristics of a high-pressure-ratio turbojet engine at altitude

Effects of external stores on the static longitudinal aerodynamic characteristics of a model of a 45 degree swept-wing fighter airplane at Mach numbers of 1.61 and 2.01

The effect of leading-edge extensions on the longitudinal characteristics at Mach numbers up to 0.92 of a wing-fuselage-tail combination having a 40 degree sweptback wing with NACA 64A thickness distribution

Effect of large negative dihedral of the horizontal tail on longitudinal and lateral stability characteristics of a swept-wing configuration at transonic speeds

Effect of leading-edge droop on the aerodynamic and loading characteristics of a 4-percent-thick unswept-wing-fuselage combination at transonic speeds

Application of Tchebichef form of harmonic analysis to the calculation of zero-lift wave drag of wing-body-tail combinations

Application of area suction to leading-edge and trailing-edge flaps on a 44 degree swept-wing model

Spreading characteristics of a jet expanding from choked nozzles at Mach 1.91

Static longitudinal and lateral stability characteristics at low speed of unswept-midwing models having wings with an aspect ratio of 2, 4, or 6

Full-scale wind-tunnel tests of a 35 degree swept-wing fighter airplane with a spoiler-slot-deflector lateral control system

Comparison of experimental and theoretical normal-force distributions (including Reynolds number effects) on an ogive-cylinder body at Mach number 1.98

Comparison of the experimental and theoretical distributions of lift on a slender inclined body of revolution at M = 2

Wind-tunnel investigation of an external-flow jet-augmented slotted flap suitable for application to airplanes with pod-mounted jet engines

A study of a missile designed to fly at low speed with its longitudinal axis aligned with the flight path


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