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- Turbojet combustor performance with injection of hydrogen peroxide for thrust augmentation
- Internal performance characteristics of short convergent-divergent exhaust nozzles designed by the method of characteristics
- An analog study of a shock-position diffuser control on a supersonic turbojet engine
- Some recent research on the handling qualities of airplanes
- Dynamics of a supersonic inlet with adjustable bypass in combination with a J34 turbojet engine
- Flight determination of drag and pressure recovery of two scoop inlets located at maximum-body-diameter station at Mach numbers from 0.8 to 1.8
- The use of the horizontal tail for roll control
- Factors affecting the maximum lift-drag ratio at high supersonic speeds
- Spinning and related problems at high angles of attack for high-speed airplanes
- Effects of wing-body geometry on the lateral-flow angularities at subsonic speeds
- A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver
- Flutter investigation at low speed of a 40 degree sweptback wing with pylon-mounted stores, tested as a semispan-cantilever wing and as a full-span wing on a towed airplane model
- A wind-tunnel investigation of the development of lift on wings in accelerated longitudinal motion
- Wind-tunnel investigation of damping in roll at supersonic speeds of triangular wings at angles of attack
- A variable-geometry annular cascade-type inlet at Mach numbers of 1.9 and 3.05
- Theoretical prediction of the side force on stores attached to configurations traveling at supersonic speeds
- Wind-tunnel investigation of the static longitudinal and lateral stability of a 1/62-scale model of the X-1E at supersonic speeds
- Transonic investigation at lifting conditions of streamline contouring in the sweptback-wing-fuselage juncture in combination with the transonic area rule
- A flight and analytical study of methods for reducing automatic-interceptor tracking errors caused by target maneuvers
- Flight and analytical study of roll requirements of a fighter airplane
- Effects of two leading-edge modifications on the aerodynamic characteristics of a thin low-aspect-ratio delta wing at transonic speeds
- An Experimental Investigation of Sting-Support Effects on Drag and a Comparison with Jet Effects at Transonic Speeds
- Lift, Drag, Static Stability, and Buffet Boundaries of a Model of the McDonnell F3H-1N Airplane at Mach Numbers from 0.40 to 1.27, TED No. NACA DE 351
- Longitudinal and Lateral Stability, Control Characteristics, and Vertical-Tail-Load Measurements for 0.03-Scale Model of the Avro CF-105 Airplane at Mach Number 1.41
- Concluding Report on Free-Spinning and Recovery Characteristics of a 1/24-Scale Model of the Grumman F11F-1 Airplane, TED No. NACA AD 395
- Ditching Investigation of a 1/12-Scale Model of the Douglas F4D-1 Airplane, TED No. NACA DE 384
- Transonic investigation of aerodynamic characteristics of a swept-wing fighter-airplane model with leading-edge droop in combination with outboard chord-extensions and notches
- An investigation of the hydrodynamic characteristics of a dynamic model of a transonic seaplane design having a planing-tail hull
- Low-speed static stability characteristics of a cambered-delta-wing model
- Lift-curve slopes determined in flight on a flexible swept-wing jet bomber
- Investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections
- The Interference Effects of a Body on the Spanwise Load Distributions of Two 45 Degree Sweptback Wings of Aspect Ratio 8.02 from Low-Speed Tests
- Operation of an experimental air-cooled turbojet engine at turbine-inlet temperatures from 2200 R to 2935 R
- Impingement of Droplets in 60 Degree Elbows with Potential Flow
- An Analysis of Air-turborocket Engine Performance Including Effects of Component Changes
- Summary of NACA Research on Afterburners for Turbojet Engines
- Turbojet Performance and Operation at High Altitudes With Hydrogen and JP-4 Fuels
- Performance characteristics of an underslung vertical-wedge inlet with porous suction at Mach numbers of 0.63 and 1.5 to 2.0
- Performance of a Blunt-lip Side Inlet With Ramp Bleed, Bypass, and a Long Constant-area Duct Ahead of the Engine- Mach Numbers 0.66 and 1.5 to 2.1
- Investigation of heat transfer from a stationary and rotating ellipsoidal forebody of fineness ratio 3
- Analysis of turbojet and ram-jet engine cycles using various fuels
- Use of Truncated Flapped Airfoils for Impingement and Icing Tests of Full-Scale Leading-Edge Sections
- Performance of a Short Combustor at High Altitudes Using Hydrogen Fuel
- Investigation of the air-flow-regulation characteristics of a translating-spike inlet with two oblique shocks from Mach 1.6 to 2.0
- Instrumentation for measurements of free-space sound pressures in the immediate vicinity of a propeller in flight
- Interaction of grids with traveling shock waves
- Initial results of a flight investigation of a gust-alleviation system
- Investigation of plastic behavior of binary aluminum alloys by internal-friction methods
- A method for obtaining statistical data on airplane vertical velocity at ground contact from measurements of center-of-gravity acceleration
- The nickel dip : a radioisotope study of metallic deposits in porcelain enameling