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- Effect on the low-speed aerodynamic characteristics of a 49 degree sweptback wing having an aspect ratio of 3.78 of blowing air over the trailing-edge flap and aileron
- Evaluation of Altitude-Ignition Characteristics of Three Fuels of Different Volatility in a Turbojet Engine
- Effects of two spinner shapes on the pressure recovery in an NACA 1-series D-type cowl behind a three-blade propeller at Mach numbers up to 0.80
- Experimental determination of boundary-layer transition on a body of revolution at M = 3.5
- Experimental data for four full-scale conical cooling-air ejectors
- Experimental determination of aerodynamic forces normal to the chord due to rotating stall acting on compressor blading
- An experimental investigation of four triangular-wing-body combinations in sideslip at Mach numbers 0.6, 0.9, 1.4, and 1.7
- Experimental investigation of control signals and the nature of stall and surge behavior in a turbojet engine
- Experimental investigation of effect of high-aspect-ratio rotor blades on performance of conservatively designed turbine
- Experimental investigation of the effect of a shrouded rotor on the performance of a conservatively designed turbine
- Experimental investigation of the effect of fuel-injection-system design variables on afterburner performance
- Experimental investigation of the aerodynamic characteristics of a ballistic-type missile
- Aerodynamic characteristics at transonic and supersonic speeds of a rocket-propelled airplane configuration having a 52.5 degree delta wing and a low, swept horizontal tail
- Aerodynamic characteristics including effects of wing fixes of a 1/20-scale model of the Convair F-102 airplane at transonic speeds
- Aerodynamic characteristics of a cruciform-wing missile with canard control surfaces and of some very small span wing-body missiles at a Mach number of 1.41
- Aerodynamic characteristics of a full-span trailing-edge control on a 60 degree delta wing with and without a spoiler at Mach number 1.61
- Effect of inlet-annulus area blockage on over-all performance and stall characteristics of an experimental 15-stage axial-flow compressor
- Multiple over-all performance and rotating-stall characteristics of a 15-stage experimental axial-flow compressor at an intermediate speed
- Summary of rocket-model tests at zero lift of an arrow-wing missile configuration from Mach numbers of 0.9 to 1.8
- Results of free-flight test of 1/10-scale model of the Convair XF2Y-1 airplane between Mach numbers of 0.7 and 1.45, including power-on flight at Mach number 1.2 : TED No. NACA DE 365
- Shock-turbulence interaction and the generation of noise
- Some screeching-combustion characteristics of a transpiration-cooled afterburner having a porous wall of wire cloth
- Some observations of shock-induced turbulent separation on supersonic diffusers
- Some internal-flow characteristics of several axisymmetrical NACA 1-series nose air inlets at zero flight speed
- Starting and performance characteristics of a large asymmetric supersonic free-jet facility
- Starting characteristics and combustion performance of magnesium slurry in 6.5-inch-diameter ram-jet engine mounted in connected-pipe facility
- Pumping and thrust characteristics of several divergent cooling-air ejectors and comparison of performance with conical and cylindrical ejectors
- Tests in the Ames 40- by 80-foot wind tunnel of the aerodynamic characteristics of airplane models with plain spoiler ailerons
- The effects of wing-mounted external stores on the trim, buffet, and drag characteristics of a rocket-propelled model having a 45 degree sweptback wing
- Experimental performance of liquid fluorine-liquid ammonia propellant combination in 1000-pound-thrust rocket engines
- Effect of a wing leading-edge flap and chord-extension on the high subsonic control characteristics of a spoiler-slot-deflector control located at two spanwise positions
- Effects of high-lift devices and horizontal-tail location on the low-speed characteristics of a large-scale 45 degree swept-wing airplane configuration
- Investigation of the effects of profile shape on the aerodynamic and structural characteristics of thin, two-dimensional airfoils at supersonic speeds
- Flight investigation of the effects of horizontal-tail height, moment of inertia, and control effectiveness on the pitch-up characteristics of a 35 degree swept-wing fighter airplane at high subsonic speeds
- Flight investigation of the effects of a partial-span leading-edge chord extension on the aerodynamic characteristics of a 35 degree swept-wing fighter airplane
- Free-flight measurements of the rolling effectiveness and operating characteristics of a bellows-actuated split-flap aileron on a 60 degree delta wing at Mach numbers between 0.8 and 1.8
- Summary of free-flight performance of a series of ram-jet engines at Mach numbers from 0.80 to 2.20
- Investigation of a 1/4-scale model of the Republic F-105 airplane in the Langley 19-foot pressure tunnel : influence of trailing-edge flap span and deflection on the longitudinal characteristics
- Investigation of a 1/4-Scale Model of the Republic F-105 Airplane in the Langley 19-Foot Pressure Tunnel: Longitudinal Stability and Control of the Model Equipped with a Supersonic-Type Elliptical Wing-Root Inlet
- Transonic wind-tunnel investigation of the effect of body indentation for boattail and cylindrical afterbody shapes on the aerodynamic characteristics of an unswept-wing-body combination
- A transonic wind-tunnel investigation of the effects of twist and camber with and without incidence, twist and body indentation on the aerodynamic characteristics of a 45 degree sweptback wing-body configuration
- A summary of information on support interference at transonic and supersonic speeds
- Altitude performance and operational characteristics of an XT38-A-2 turboprop engine
- Methods for obtaining desired helicopter stability characteristics
- Altitude-chamber investigation of J73-GE-1A turbojet engine component performance
- Altitude investigation of can-type flame holder in 20-inch-diameter ram-jet combustor
- The transonic aerodynamic characteristics of structurally related wings of low aspect ratio having a spanwise variation in thickness ratio-transonic bump technique
- Altitude performance characteristics of the J73-GE-1A turbojet engine
- Altitude performance of compressor, turbine, and combustor components of 600-B9 turbojet engine
- Altitude performance of compressor, combustor, and turbine components of XT38-A-2 turboprop engine