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A review of the thermodynamic, transport, and chemical reaction rate properties of high-temperature air

Effects of canards on airplane performance and stability

Forces and pitching moments on an aspect-ratio-3.1 wing-body combination at Mach numbers from 2.5 to 3.5 and sublimation studies of the effect of single-elements roughness on the boundary-layer flow

Thermal fatigue of ductile materials 1: effect of variations in the temperature cycle on the thermal-fatigue of S-816 and inconel 550

Theoretical and experimental analysis of the reduction of rotor blade vibration in turbomachinery through the use of modified stator vane spacing

Thermal reaction of diborane with trimethylborane

Thermal fatigue of ductile materials 2: effect of cyclic thermal stressing on the stress-rupture life and ductility of S-816 and Inconel 550

Mechanism of beneficial effects of boron and zirconium on creep-rupture properties of a complex heat-resistant alloy

An experimental study of the turbulent boundary layer on a shock-tube wall

On solutions for the transient response of beams

Low tip Mach number stall characteristics and high tip Mach number compressibility effects on a helicopter rotor having an NACA 0009 tip airfoil section

Vibration survey of four representative types of air-cooled turbine blades

Comparison of Calculated and Experimental Temperatures and Coolant Pressure Losses for a Cascade of Small Air-Cooled Turbine Rotor Blades

Effects of compressibility on rotor hovering performance and synthesized blade-section characteristics derived from measured rotor performance of blades having NACA 0015 airfoil tip sections

Matrix method for obtaining spanwise moments and deflections of torsionally rigid rotor blades with arbitrary loadings

Maximum theoretical tangential velocity component possible from straight-back converging and converging-diverging stators at supercritical pressure ratios

A study of several theoretical methods for computing the zero-lift wave drag of a family of open-nosed bodies of revolution in the Mach number range of 2.0 to 4.0

A phenomenological theory for the transient creep of metals at elevated temperatures

High-speed landing loads measured on the Douglas X-3 research airplane

The effects of a modified roll-command system on the flight-path stability and tracking accuracy of an automatic interceptor

Discharge coefficients for combustor-liner air-entry holes II : flush rectangular holes, step louvers, and scoops

Investigation of effects of distributed surface roughness on a turbulent boundary layer over a body of revolution at a mach number of 2.01

Exploratory Wind-Tunnel Investigation to Determine the Lift Effects of Blowing over Flaps from Nacelles Mounted Above the Wing

Compilation of information on the transonic attachment of flows at the leading edges of airfoils

Theoretical analysis of the interference effects of several supersonic-tunnel walls capable of absorbing the shock caused by the nose of a model

A theoretical analysis of the effect of engine angular momentum on longitudinal and directional stability in steady rolling maneuvers

Graphs of reduced variables for computing histories of vaporizing fuel drops, and drop histories under pressure

Experimental study of the equivalence of transonic flow about slender cone-cylinders of circular and elliptic cross section

Ground reflection of jet noise

Effects of airplane flexibility on wing strains in rough air at 35,000 feet as determined by a flight investigation of a large swept-wing airplane

A fuselage addition to increase drag-rise Mach number of subsonic airplanes at lifting conditions

Hypersonic viscous flow over slender cones

Friction studies of various materials in liquid nitrogen

Friction and wear with reactive gases at temperatures up to 1200 F

Free-spinning-tunnel investigation of a 1/28-scale model of the North American FJ-4 airplane: TED No. NACA AD-3112

Heat transfer in isotropic turbulence during the final period of decay

Heat-transfer and pressure measurements on flat-faced cylinders at a Mach number of 2

Heat transfer and thermal stresses in sandwich panels

Comparison of hydrodynamic-impact acceleration and response for systems with single and with multiple elastic modes

Operational problems of manned orbital vehicles

Large-scale wind-tunnel tests of an airplane model with a 45 degree sweptback wing of aspect ratio 2.8 employing high-velocity blowing over the leading- and trailing-edge flaps

Large-scale wind-tunnel tests of a jet-transport-type model with leading- and trailing-edge high-lift devices

Normal component of induced velocity for entire field of a uniformly loaded lifting rotor with highly swept wake as determined by electromagnetic analog

Flow induced by a rotor in power-on vertical descent

Effect of favorable pressure gradients on transition for several bodies of revolution at Mach 3.12

Effect of environments of sodium hydroxide, air, and argon on the stress-rupture properties of nickel at 1500 F

Effect of fiber orientation in races and balls under rolling-contact fatigue conditions

Effect of control trailing-edge thickness or aspect ratio on the oscillating hinge-moment and flutter characteristics of a flap-type control at transonic speeds

Effect of flow incidence and Reynolds number on low-speed aerodynamic characteristics of several noncircular cylinders with applications to directional stability and spinning

Effect of fuel-orifice diameter on performance of heptane-oxygen rocket-engines


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