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- Intensity, scale, and spectra of turbulence in mixing region of free subsonic jet
- Investigation of the aerodynamic characteristics of a model wing-propeller combination and of the wing and propeller separately at angles of attack up to 90 degrees
- Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition
- The near noise field of static jets and some model studies of devices for noise reduction
- Comparison of several methods for obtaining the time response of linear systems to either a unit impulse or arbitrary input from frequency-response data
- A low-speed experimental investigation of the effect of a sandpaper type of roughness on boundary-layer transition
- On the Kernel function of the integral equation relating lift and downwash distributions of oscillating wings in supersonic flow
- Effect of chord size on weight and cooling characteristics of air-cooled turbine blades
- Static Longitudinal and Lateral Stability and Control Data Obtained from Tests of a 1/15-Scale Model of the Goodyear XZP5K Airship, TED No. NACA DE 211
- Hovering-flight tests of a model of a transport vertical-take-off airplane with tilting wing and propellers
- Component performance investigation of J71 experimental turbine I : over-all performance with 97-percent-design stator areas
- The proper combination of lift loadings for least drag on a supersonic wing
- Effect of Wing Height and Dihedral on the Lateral Stability Characteristics at Low Lift of a 45 Deg Swept-Wing Airplane Configuration as Obtained from Time-Vector Analyses of Rocket-Propelled-Model Flights at Mach Numbers from 0.7 to 1.3
- Propagation of a free flame in a turbulent gas stream
- Some possibilities of using gas mixtures other than air in aerodynamic research
- Studies of the speed stability of a tandem helicopter in forward flight
- Spark ignition of flowing gases
- The response of an airplane to random atmospheric disturbances
- Boundary Layer
- Exploratory investigation of boundary-layer transition on a hollow cylinder at a Mach number of 6.9
- Theoretical calculation of the power spectra of the rolling and yawing moments on a wing in random turbulence
- Theoretical and experimental investigation of the effect of tunnel walls on the forces on an oscillating airfoil in two-dimensional subsonic compressible flow
- Theoretical investigation of flutter of two-dimensional flat panels with one surface exposed to supersonic potential flow
- Theory of wing-body drag at supersonic speeds
- Zero-angle-of-attack performance of two-dimensional inlets near Mach number 3
- Theoretical span load distributions and rolling moments for sideslipping wings of arbitrary plan form in incompressible flow
- Methods for obtaining desired helicopter stability characteristics and procedures for stability predictions
- High-temperature oxidation and ignition of metals
- Average properties of compressible laminar boundary layer on flat plate with unsteady flight velocity
- A study of the zero-lift drag-rise characteristics of wing-body combinations near the speed of sound
- An evaluation of four experimental methods for measuring mean properties of a supersonic turbulent boundary layer
- Summary of NACA research on afterburners for turbojet engines
- Axially symmetric shapes with minimum wave drag
- A wind-tunnel test technique for measuring the dynamic rotary stability derivatives at subsonic and supersonic speeds
- Exhaust Nozzles for Supersonic Flight with Turbojet Engines
- A special method for finding body distortions that reduce the wave drag of wing and body combinations at supersonic speeds
- Lift hysteresis at stall as an unsteady boundary-layer phenomenon
- Ditching investigations of dynamic models and effects of design parameters on ditching characteristics
- Extrapolation techniques applied to matrix methods in neutron diffusion problems
- A theoretical and experimental study of planing surfaces including effects of cross section and plan form
- Laminar Flow About a Rotating Body of Revolution in an Axial Airstream
- An analysis of the stability and ultimate compressive strength of short sheet-stringer panels with special reference to the influence of the riveted connection between sheet and stringer
- An investigation of forward-located fixed spoilers and deflectors as gust alleviators on an unswept-wing model
- Force, moment, and pressure-distribution characteristics of rectangular wings at high angles of attack and supersonic speeds
- Exploratory investigation of the effectiveness of biplane wings with large-chord double slotted flaps in redirecting a propeller slipstream downward for vertical take-off
- Flight determination of the lateral handling qualities of the Bell X-5 research airplane at 58.7 degrees sweepback
- Flight measurements of the low-speed characteristics of a 35 degree swept-wing airplane with area suction boundary-layer control on the flaps
- Flight-determined transonic lift and drag characteristics of the YF-102 airplane with two wing configurations
- Flight tests at supersonic speeds to determine the effect of taper on the zero-lift drag of sweptback low-aspect-ratio wings
- Flight measurements of the vibrations encountered by a tandem helicopter and a method for measuring the coupled response in flight