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- A systematic study of the effects of leading-edge chord-extensions on the low-speed longitudinal stability characteristics of three 45 degree sweptback wings
- Some studies of axisymmetric free jets exhausting from sonic and supersonic nozzles into still air and into supersonic streams
- Steady-state and surge characteristics of a compressor equipped with variable inlet guide vanes operating in a turbojet engine
- Statistical measurements of landing-contact conditions of a heavy bomber
- Summary of the flight conditions and maneuvers in which maximum wing and tail loads were experienced on a swept-wing fighter airplane
- Simplified procedures for estimating flap-control loads at supersonic speeds
- A study of flame-holder elements for use in high-velocity afterburners
- Statistical measurements of landing contact conditions of the Boeing B-47 airplane
- Simulator studies of a simple homing system
- Static longitudinal and lateral stability and control characteristics of a model of a 35 degree swept-wing airplane at a Mach number of 1.41
- Static longitudinal and lateral stability and control characteristics of an 0.065-scale model of the Chance Vought Regulus II missile at Mach numbers of 1.41, 1.61, and 2.01 : TED No. NACA AD 398
- Static longitudinal and lateral stability and control data from an exploratory investigation at a Mach number of 6.86 of an airplane configuration having a wing of trapezoidal plan form
- Static longitudinal and lateral stability data from an exploratory investigation at Mach number 4.06 of an airplane configuration having a wing of trapezoidal plan form
- Static longitudinal and lateral stability and control characteristics of an airplane configuration having a wing of trapezoidal plan form with various tail airfoil sections and tail arrangements at a Mach number of 6.86
- Removal of secondary-flow accumulations in a two-dimensional turbine nozzle passage by boundary-layer bleed
- An experimental study of a method for designing fuselage side air inlets for high performance at transonic and low supersonic speeds
- Effects of free-flight rocket-model booster-adapter configurations on the aerodynamic characteristics in pitch and sideslip of a swept-wing fighter airplane model at a Mach number of 2.01
- Ignition-delay determinations of furfuryl alcohol and mixed butyl mercaptans with various white fuming nitric acids using modified open-cup and small-scale rocket engine apparatus
- Flight investigation of pentaborane fuel in 9.75-inch-diameter ram-jet engine at low equivalence ratio
- Investigation at Mach numbers of 1.41, 1.61, and 1.82 of two variable-geometry inlets having two-dimensional compression surfaces
- Investigation at supersonic speeds of external-drag effects and pumping characteristics of a short ejector
- A theory for predicting the flow of real gases in shock tubes with experimental verification
- Turboprop-engine design considerations II : design requirements and performance of turboprop engines with a single-spool high-pressure-ratio compressor
- The use of metallic inhibitors for eliminating mass transfer and corrosion in nickel and nickel alloys by molten sodium hydroxide
- Turbojet engine investigation of effect of thermal shock induced by external water-spray cooling on turbine blades of five high-temperature alloys
- Turboprop-engine design considerations I : effect of mode of engine operation on performance of turboprop engine with current compressor pressure ratio
- Transonic wind-tunnel investigation of the effects of external stores and store position on the aerodynamic characteristics of a 1/16-scale model of the Douglas D-558-II research airplane
- Transonic wind-tunnel investigation of the effects of taper ratio and body indentation on the aerodynamic loading characteristics of a 45 degree sweptback wing in the presence of a body
- Tank investigation of the hydrodynamic characteristics of a 1/3.33-scale jet-powered dynamic model of the Martin XP6M-1 flying boat with a revised forebody planing bottom : TED No. NACA DE 385
- Altitude component performance of the YJ73-GE-3 turbojet engine
- Turbulent-heat-transfer measurements at a Mach number of 2.06
- Turbulent-heat-transfer measurements at a Mach number of 0.87
- Additional experimental heat-transfer and durability data on several forced-convection, air-cooled, strut-supported turbine blades of improved design
- Adaptation of Combustion Principles to Aircraft Propulsion, Volume 1, Basic Considerations in the Combustion of Hydrocarbon Fuels with Air
- Additional comparisons between computed and measured transonic drag-rise coefficients at zero lift for wing-body-tail configurations
- Aerodynamic and hydrodynamic characteristics of models of some aircraft-towed mine-sweeping devices : TED No. NACA AR 8201
- Aerodynamic characteristics and pressure distributions of a 6-percent-thick 49 degree sweptback wing with blowing over half-span and full-span flaps
- Additional measurements of the low-speed static stability of a configuration employing three triangular wing panels and a body of equal length
- Theoretical investigation of the effects of configuration changes on the center of pressure shift of a body-wing-tail combination due to angle of attack and Mach number at transonic and supersonic speeds
- A limited flight investigation of the effect of dynamic vibration absorbers on the response of an airplane structure during buffeting
- A limited analysis of buffeting experienced in flight by a North American F-86A-1 airplane with and without large external fuel tanks
- Low-speed study of the effects of frequency on the stability derivatives of wings oscillating in yaw with particular reference to high angle of attack conditions
- Low-speed wind-tunnel investigation of leading-edge porous suction on a 4-percent-thick 60 degree delta wing
- Minimum-drag bodies of revolution in a nonuniform supersonic flow field
- Model ditching investigation of the Boeing 707 jet transport
- Modified tubular combustor as high-temperature gas generators
- Stability and control characteristics obtained during demonstration of the Douglas X-3 research airplane
- Some aspects of the design of hypersonic boost-glide aircraft
- Performance of a high-solidity high-pressure-ratio transonic rotor
- Performance measurements from a rocket-powered exploratory research missile flown to a Mach number of 10.4