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- An experimental investigation of a flat ram-jet engine on a helicopter rotor
- Gas-turbine-engine performance when heat from liquid-cooled turbines is rejected ahead of, within, or behind main compressor
- Gas-to-blade heat-transfer coefficients and turbine heat-rejection rates for a range of one-spool cooled-turbine engine designs
- Performance characteristics of ring-cascade-type thrust reversers
- Performance of a short combustor at high altitudes using hydrogen fuel
- Investigation at high subsonic speeds of some effects of sideslip on the aerodynamic loads on finned and unfinned bodies mounted from the wing of a swept-wing-fuselage model
- Investigation at high subsonic speeds of the static lateral and directional stability and tail-loads characteristics of a model having a highly tapered swept wing of aspect ratio 3 and two horizontal-tail positions
- Investigation at high subsonic speeds of a body-contouring method for alleviating the adverse interference at the root of a sweptback wing
- Effect of fuselage circumferential inlet location on diffuser-discharge total-pressure profiles at supersonic speeds
- Effect of three design parameters on the operating characteristics of 75-millimeter-bore cylindrical roller bearings at high speeds
- The effects at a Mach number of 6.86 of drag brakes on the lift, drag, and pitching moment of an ogive cylinder
- Effects of a J34 turbojet engine on supersonic diffuser performance
- Charts for estimating the hovering endurance of a helicopter
- Discharge coefficients for combustor-liner air-entry holes
- Distribution of losses behind a compressor rotor as measured by a rotating rake
- Fatigue crack propagation in severely notched bars
- Factors affecting flow distortions produced by supersonic inlets
- Fatigue-crack-propagation and residual-static-strength results on full-scale transport-airplane wings
- Tests with hydrogen fuel in a simulated afterburner
- An experimental study of the zero-angle-of attack transonic drag associated with the vertical position of a horizontal tail at zero incidence
- Some experiments relating to the problem of simulation of hot jet engines in studies of jet effects on adjacent surfaces at a free-stream Mach number of 1.80
- A theoretical analysis of heat transfer in regions of separated flow
- The effects of blowing over various trailing-edge flaps on an NACA 0006 airfoil section, comparisons with various types of flaps on other airfoil sections, and an analysis of flow and power relationships for blowing systems
- Effect of boundary-layer control and inlet lip shape on the performance of a twin-scoop air-induction system at Mach numbers from 0 to 1.9
- Effect of camber on the drag of a body of revolution
- Free-flight investigation at transonic speeds of the stability characteristics of a tailless missile configuration having a 45 degree sweptback wing of aspect ratio 4
- Free-flight investigation over a Mach number range from 0.74 to 1.43 at lift coefficients from minus 0.15 to 0.75 of an airplane-configuration model having a 52.5 degree delta wing and a low swept horizontal tail
- Free-flight investigation at transonic speeds of drag coefficients of a boattail body of revolution with a simulated turbojet exhaust issuing at the base from conical short-length ejectors
- A free-flight investigation of the effects of a sonic jet on the total-drag and base-pressure coefficients of a boattail body of revolution from Mach number 0.83 to 1.70
- Tensile properties of AZ31A-0 magnesium-alloy sheet under rapid-heating and constant-temperature conditions
- Tensile properties of Inconel and RS-120 titanium-alloy sheet under rapid-heating and constant-temperature conditions
- Cloud-droplet ingestion in engine inlets with inlet velocity ratios of 1.0 and 0.7
- Comparison of theoretical stresses and deflections of multicell wings with experimental results obtained from plastic models
- Effects of Reynolds number and leading-edge shape on the low-speed longitudinal stability of a 6-percent-thick 45 degree sweptback wing
- Charts adapted from Van Driest's turbulent flat-plate theory for determining values of turbulent aerodynamic friction and heat-transfer coefficients
- Effects of leading-edge radius on the longitudinal stability characteristics of two 60 degree sweptback wings at high Reynolds numbers
- On possible similarity solutions for three-dimensional incompressible laminar boundary layers 2: similarity with respect to stationary polar coordinates
- Wind-tunnel investigation of the damping in roll of the Bell X-1E research airplane and its components at supersonic speeds
- Wind-tunnel investigation of the damping in roll of the Bell X-1A research airplane and its components at supersonic speeds
- Wind-tunnel investigation of the damping in roll of the Douglas D-558-II research airplane and its components at supersonic speeds
- On possible similarity solutions for three-dimensional incompressible laminar boundary layers 1: similarity with respect to stationary rectangular coordinates
- Analysis of particle motions for a class of three-dimensional incompressible laminar boundary layers
- Cross flows in laminar incompressible boundary layers
- Comparison of flight and wind-tunnel measurements of high-speed-airplane stability and control characteristics
- Qualitative study of flow characteristics through single-stage turbines as made from rotor-exit surveys
- A description of the Ames 2- by 2-foot transonic wind tunnel and preliminary evaluation of wall interference
- Wind-tunnel tests of blowing boundary-layer control with jet pressure ratios up to 9.5 on the trailing-edge flaps of a 35 degree sweptback wing airplane
- A study of the high-speed performance characteristics of 90 degrees bends in circular ducts
- A study of the efficiency of high-strength, steel, cellular-core sandwich plates in compression
- Preliminary investigation of methods to increase base pressure of plug nozzles at Mach 0.9