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- Performance evaluation of reduced-chord rotor blading as applied to J73 two-stage turbine : over-all performance with standard rotor blading at inlet conditions of 35 inches of mercury absolute and 700 R
- A preliminary investigation of methods for improving the pressure recovery characteristics of variable-geometry supersonic-subsonic diffuser systems
- Preliminary investigation of combustion of diborane in a turbojet combustor
- Preliminary investigation of propane combustion in a 3-inch-diameter duct of inlet-air temperatures of 1400 to 1600 F
- Pressure losses of titanium and magnesium slurries in pipes and pipeline transitions
- Atmospheric temperature observations to 100,000 feet for several climatological regions of the Northern Hemisphere
- Analyses for turbojet thrust augmentation with fuel-rich afterburning of hydrogen, diborane, and hydrazine
- Influence of crucible materials on high-temperature properties of vacuum-melted nickel-chromium-cobalt alloy
- The influence of imperfect radar space stabilization on the final attack phase of an automatic interceptor system
- Influence of boric oxide deposition on turbojet-engine operation
- Hinge-moment characteristics for a series of controls and balancing devices on a 60 degree delta wing at Mach numbers of 1.61 and 2.01
- Development of a piston-compressor type light-gas gun for the launching of free-flight models at high velocity
- Effect of hinge-line position on the oscillating hinge moments and flutter characteristics of a flap-type control at transonic speeds
- Free-flight experience of the lateral stability characteristics at low lift of a 45 degree swept-wing rocket-propelled model equipped with a nonlinear yaw-rate damper system at Mach numbers from 0.76 to 1.73
- Foreign-object retention and flow characteristics of retractable engine-inlet screens
- Fatigue Investigation of Full-Scale Transport-Airplane Wings: Variable-Amplitude Tests with a Gust-Loads Spectrum
- Accelerations in fighter-airplane crashes
- Effect of standing transverse acoustic oscillations on fuel-oxidant mixing in cylindrical combustion chambers
- Effect of sweep on performance of compressor blade sections as indicated by swept-blade rotor, unswept-blade rotor, and cascade tests
- Hydrogen-oxygen explosions in exhaust ducting
- Analog computer study of some filtering, command-computer, and automatic-pilot problems connected with the attack phase of the automatically controlled supersonic interceptor
- Experimental investigation of an axial-flow-compressor inlet stage operating at transonic relative inlet Mach numbers V : rotor blade-element performance at a reduced blade angle
- Experimental investigation of attenuation of strong shock waves in a shock tube with hydrogen and helium as driver gases
- Experimental investigation of performance of single-stage transonic compressor with guide vanes turning counter to direction of rotor whirl
- Jet effects on the drag of conical afterbodies for Mach numbers of 0.6 to 1.28
- Design and performance of flight-type liquid-hydrogen heat exchanger
- Investigation of the effect of velocity diagram on inlet total-pressure distortions through single-stage subsonic axial-flow compressors
- Internal performance of several auxiliary air inlets immersed in a turbulent boundary layer at Mach numbers of 1.3, 1.5, and 2.0
- Experimental performance of a 5000-pound-thrust rocket chamber using a 20-percent-fluorine-80-percent-oxygen mixture with RP-1
- Experimental study of the effects of scale on the absolute values of zero-lift drag of aircraft configurations at transonic speeds
- Performance of external-internal compression inlet with abrupt internal turning at Mach numbers 3.0 to 2.0
- Preliminary investigation of the combustion of a 50 percent pentaborane - 50 percent JP-4 fuel blend in a turbojet combustor at simulated altitude conditions
- Oblique-shock relations at hypersonic speeds for air in chemical equilibrium
- Some effects of tail height and wing plan form on the static longitudinal stability characteristics of a small-scale model at high subsonic speeds
- A study of injection processes for liquid oxygen and gaseous hydrogen in a 200-pound-thrust rocket engine
- A study of temperature transients at the inlet of a turbojet engine
- Preliminary performance evaluation of blends of pentaborate and JP-4 fuel in a full-scale turbojet engine
- A review of the physical and thermodynamic properties of boric oxide
- Some effects of valve friction and shock stick friction on control quality in a helicopter with hydraulic-power control systems
- Thermodynamic study of a Roots compressor as a source of high-temperature air
- Thin airfoil theory based on approximate solution of the transonic flow equation
- Wind-tunnel tests of the static longitudinal characteristics at low speed of a swept-wing airplane with blowing flaps and leading-edge slats
- Wind-tunnel tests of the static longitudinal characteristics at low speed of a swept-wing airplane with slotted flaps, area-suction flaps, and wing leading-edge devices
- Analytical and experimental investigation of the effects of compressor interstage air bleed on performance characteristics of a 13-stage axial-flow compressor
- An analysis of vertical-tail loads measured in flight on a swept-wing bomber airplane
- Analysis of two-spool turboprop-engine characteristics
- Wind-tunnel investigation of the aerodynamic characteristics of a series of swept, highly tapered thin wings at transonic speeds: transonic bumb method
- Wind-tunnel investigation of the static lateral stability characteristics of wind-fuselage combinations at high subsonic speeds: Taper-ratio series
- Aerodynamic load distribution over a 45 degree swept wing having a spoiler-slot-deflector aileron and other spoiler ailerons for Mach numbers from 0.60 to 1.03
- Aerodynamic and hydrodynamic characteristics of a proposed supersonic multijet water-based hydro-ski aircraft with a variable-incidence wing