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- Review of experimental investigations of liquid-metal heat transfer
- A reevaluaion of data on atmospheric turbulence and airplane gust loads for application in spectral calculations
- A relation between burning velocity and quenching distance
- Analysis of cooling-air requirements of corrugated-insert-type turbine blades suitable for a supersonic turbojet engine
- Wind-tunnel investigation at low speeds to determine the effect of aspect ratio and end plates on a rectangular wing with jet flaps deflected 85 degrees
- Wear of typical carbon-base sliding seal materials at temperatures to 700 F
- Weight-flow and thrust limitations due to use of rotating combustors in a turbojet engine
- Calculation of the forces and moments on a slender fuselage and vertical fin penetrating lateral gusts
- Calculation and compilation of the unsteady-lift functions for a rigid wing subjected to sinusoidal gusts and to sinusoidal sinking oscillations
- Temperatures in a J47-25 turbojet-engine turbine section during steady-state and transient operation in an altitude test stand
- Comparison between experimental and predicted downwash at a Mach number of 0.25 behind a wing-body combination having a triangular wing of aspect ratio of 2.0
- Thermal stability of pentaborane in the range 329 to 419 F
- A factor affecting transonic leading-edge flow separation
- On slender-body theory and the area rule at transonic speeds
- The effects upon body drag of jets exhausting from wing-mounted nacelles
- 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