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- Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers 0.6 to 1.4
- Correlation of flight and analog investigations of roll coupling
- Preliminary attempts at isothermal compression of a supersonic air stream
- Investigation at supersonic and subsonic Mach numbers of auxiliary inlets supplying secondary air flow to ejector exhaust nozzles
- Effect of diameter of closed-end coolant passages on natural-convection water cooling of gas-turbine blades
- Criteria for initial flow reversal in symmetrical twin-intake air-induction systems operating at supersonic speeds
- Visual study of free convection in a narrow vertical enclosure
- 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
- 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
- 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
- Wind-tunnel investigation of the static longitudinal and lateral stability of a 1/62-scale model of the X-1E at supersonic speeds
- 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
- 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
- Effects of wing-tip droop on the longitudinal characteristics of two highly swept wing-body combinations at Mach numbers from 0.6 to 1.4
- A buffet investigation at high subsonic speeds of wing-fuselage-tail combinations having sweptback wings with NACA 64A thickness distributions, fences, a leading-edge extension, and body contouring
- A study of liquid boric oxide particle growth rates in a gas stream from a simulated jet engine combustor
- Theoretical analysis of total-pressure loss and airflow distribution for tubular turbojet combustors with constant annulus and liner cross-sectional areas
- Investigation of an asymmetric "penshape" exit having circular projections and discharging into quiescent air
- An inlet design concept to reduce flow distortion at angle of attack
- Evaluation of the use of electrical resistance for detecting overtemperatured S-816 turbine blades
- Survey of hydrogen combustion properties
- Airplane motions and loads induced by flying through the flow field generated by an airplane at low supersonic speeds
- Flight investigation of a ram jet burning magnesium slurry fuel and having a conical shock inlet designed for a Mach number of 4.1
- Investigation of transonic flutter characteristics of a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6
- Flutter at very high speeds
- Effects on adjacent surfaces from the firing of rocket jets
- Span loadings due to wing twist at transonic and supersonic speeds
- Investigation at Mach numbers from 0.80 to 1.43 of pressure and load distributions over a thin 45©� sweptback highly tapered wing in combination with basic and indented bodies
- Aerodynamic characteristics of a spoiler-slot-deflector control on a 45©� sweptback wing at Mach numbers of 1.61 and 2.01
- Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers
- Investigation of the aerodynamic characteristics in pitch and sideslip of a 45©� swept-wing airplane configuration with various vertical locations of the wing and horizontal tail.Static lateral and directional stability; Mach numbers of 1.41 and 2.01
- Theoretical rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming frozen composition
- Preliminary investigation of shield to improve angle-of-attack performance of nacelle-type inlet
- Stability of two rocket-propelled models having aspect-ratio-5 unswept tails on a long body for the Mach number range of 1.7 to 2.4
- Transonic wind-tunnel investigation of aerodynamic-loading characteristics of a 2-percent-thick trapezoidal wing in combination with basic and indented bodies