Browse TRAIL Inventories

Experimental investigation at Mach numbers from 0 to 1.9 of trapezoidal and circular side inlets for a fighter-type airplane

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections II : blade-element performance

Experimental investigation of a transonic compressor rotor with a 1.5-inch chord length and an aspect ratio of 3.0 II : blade-element performance

Experimental flutter investigation of a thin unswept wing at transonic speeds

Experimental performance of fluorine-oxygen with JP4 fuel in a rocket engine

An experimental investigation of two methods for reducing transonic drag of swept-wing and body combinations

Experimental investigation of a surge control on a turbojet engine

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections III : comparison of blade-element performance with three levels of solidity

Experimental investigation of a transonic compressor rotor with a 1.5-inch chord length and an aspect ratio of 3.0 I : design, over-all performance, and rotating-stall characteristics

Flight measurements of directional stability to a Mach number of 1.48 for an airplane tested with three different vertical tail configurations

Free-flight investigation to obtain drag-at-lift and stability data for a 60 degree delta-wing-body configuration over a Mach number range of 1.3 to 1.6

Flight measurements of base pressure on bodies of revolution with and without simulated rocket chambers

Flight Measurements of Elevon Hinge Moments on the XF-92A Delta-Wing Airplane

Flight Measurements of Horizontal-Tail Loads on the Bell X-5 Research Airplane at a Sweep Angle of 58.7 Degrees

Effect of outer-shell design on performance characteristics of convergent-plug exhaust nozzles

Effects of several geometric variables on internal performance of short convergent-divergent exhaust nozzles

Investigation of boattail and base pressures of twin-jet afterbodies at Mach number 1.91

Effect of area-suction-type boundary-layer control on the landing-approach characteristics of a 35 degree swept-wing fighter

Comparison of two methods of modulating the throat area of convergent plug nozzles

Free-spinning-tunnel investigation to determine the effect of spin-recovery rockets and thrust simulation on the recovery characteristics of a 1/25-scale model of the Chance Vought XF8U-1 airplane: TED No. NACA DE 392

The effects of flexibility on the longitudinal and lateral directional response of a large airplane

A comparison of the maneuvering performance of a monowing versus a cruciform missile

The effect of leading-edge droop upon the pressure distribution and aerodynamic loading characteristics of a 45 degree sweptback wing at transonic speeds

The effect of blunt-trailing-edge elevons on the longitudinal and lateral handling qualities of the semitailless airplane

Effect of rotor leading-edge sweepback on performance of a transonic turbine

Description and bibliography of NACA research on wing controls: January 1946 - February 1955

Design and performance of a 1400-foot-per-second-tip-speed supersonic compressor rotor

Effects of spanwise location of sweep discontinuity on the low-speed longitudinal stability characteristics of a complete model with wings of M and W plan form

Effects of spanwise location of sweep discontinuity on the low-speed static lateral stability characteristics of a complete model with wings of M and W plan form

A method for evaluating the loads and controllability aspects of the pitch-up problem

Application of non-afterburning turbojets to supersonic flight

Application of statistical theory to beam-rider guidance in the presence of noise 1: Wiener filter theory

Application of wing-body theory to drag reduction at low supersonic speeds

Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 2

Investigation of some wake vortex characteristics of an inclined ogive-cylinder body at Mach number 1.98

Wind-tunnel investigation at Mach 1.9 of multijet-missile base pressures

Performance of four experimental high btu-per-gallon fuels in a single turbojet combustor

Performance of a supersonic compressor with swept and tilted diffuser blades

Matching of auxiliary inlets to secondary-air requirements of aircraft ejector exhaust nozzles

Some design implications of the effects of aerodynamic heating

Spark ignition of flowing gases 5: application of fuel-air-ratio and initial-temperature data to ignition theory

A special method for finding body distortions that reduce the wave drag of wing and body combinations at supersonic speeds

Panel-flutter investigation at supersonic speeds of a pressurized structure fabricated of 0.020-inch-thick laminated glass-plastic

Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines 4: coolant-flow requirements and performance of engines using air-cooled corrugated-insert blades

Analytical comparison of convection-cooled turbine blade cooling-air requirements for several radial gas-temperature profiles

Wind-tunnel investigation at low speed of a wing having 63 degree sweepback and a drooped tip

Performance characteristics of axisymmetric two-cone and isentropic nose inlets at Mach number 1.90

A variable-geometry axisymmetric supersonic inlet with telescoping centerbody

Downwash survey behind two low-aspect-ratio variable-incidence wings in combination with three different size fuselages at a Mach number of 0.25

Theoretical analysis of the longitudinal behavior of an automatically controlled supersonic interceptor during the attack phase


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