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- A simulator study of some longitudinal stability and control problems of a piloted aircraft in flights to extreme altitude and high speed
- Simulated flight investigation of scaled-speed elastic swept-wing bomber and fighter models coupled wing tip to wing tip
- A simulation study of a wingless missile
- Static lateral and directional stability and control characteristics of revised 1/22-scale model of the Republic F-105 airplane at Mach numbers of 1.41 and 2.01 : COORD No. AF-163
- Static lateral and directional stability and control characteristics of a 1/15-scale model of the Grumman F11F-1 airplane at Mach numbers of 1.41, 1.61, and 2.01 : TED No. NACA DE 390
- Results of a flight investigation to determine the zero-lift drag characteristics of a 60 degree delta wing with NACA 65-006 airfoil section and various double-wedge sections at Mach numbers from 0.7 to 1.6
- Static longitudinal stability and control characteristics of a model of a 45 degree swept-wing fighter airplane at Mach numbers of 1.41, 1.61, and 2.01
- Static stability and control characteristics of a 0.04956-scale-model of the Convair F-102A airplane at transonic speeds
- Static lateral-directional stability characteristics of five contemporary airplane models from wind-tunnel tests at high subsonic and supersonic speeds
- Static longitudinal and lateral stability characteristics including effects of transonic area rule and wing modification of a 0.10-scale model of the Douglas A4D-1 airplane at transonic speeds: TED No. NACA AD 3114
- Proposed initiating system for crash-fire prevention systems
- Relation of turbojet propulsion system development to the strategic bomber mission
- Summary of Scale-model thrust-reverser investigation
- Section characteristics of the NACA 0006 airfoil with leading-edge and trailing-edge flaps
- Study of ram-air heat exchangers for reducing turbine cooling-air temperature of a supersonic aircraft turbojet engine
- A study of several factors affecting the stability contributed by a horizontal tail at various vertical positions on a sweptback-wing airplane model
- Study of size effect in sheet-stringer panels
- Altitude performance evaluation of J71-A-11 turbojet engine
- A horizontal-tail arrangement for counteracting static longitudinal instability of sweptback wings
- Lift and pitching-moment interference between a pointed cylindrical body and triangular wings of various aspect ratios at Mach numbers of 1.50 and 2.02
- Ignition delays and fluid properties of several fuels and nitric acid oxidants in temperature range from 70 to -105 degrees Fahrenheit
- Flight investigation of the effect of vertical-tail size on the rolling behavior of a swept-wing airplane having lateral-longitudinal coupling
- Investigation at supersonic speeds of the effects of bomb-bay configuration upon the aerodynamic characteristics of fuselages with noncircular cross sections
- Investigation by the transonic-bump method of a 35 degree sweptback semispan model equipped with a flap operated by a series of servovanes located ahead of and geared to the flap
- An investigation at subsonic speeds of several modifications to the leading-edge region of the NACA 64A010 airfoil section designed to increase maximum lift
- Investigation at zero forward speed of a leading-edge slat as a longitudinal control device for vertically rising airplanes that utilize the redirected-slipstream principle
- An investigation at Mach numbers of 1.41 and 2.01 of the aerodynamic characteristics of a swept-wing supersonic bomber configuration
- Theoretical calculation of the power spectra of the rolling and yawing moments on a wing in random turbulence
- A theory for stability and buzz pulsation amplitude in ram jets and an experimental investigation including scale effects
- Transonic wind-tunnel investigation of the effects of indentation on the wing loads of a 45 degree sweptback wing-body combination
- Transonic wind-tunnel measurements of static lateral and directional stability and vertical-tail loads for a model with a 45 degree sweptback wing
- Tank investigation of a series of related hydro-skis as load-alleviation devices for landing a seaplane in waves
- Summary of derived gust velocities obtained from measurements within thunderstorms
- Tank tests of a 1/8-size powered dynamic model of the Martin PBM-5 seaplane equipped with a single Edo hydro-ski : TED No. NACA AD3110
- Thermal decomposition of ethylpentaborane in gas phase
- Aerodynamic principles for the design of jet-engine induction systems
- Aerodynamic loadings associated with swept and unswept spoilers on a flat-plate at Mach numbers of 1.61 and 2.01
- A theoretical study of the lifting efficiency at supersonic speeds of wings utilizing indirect lift induced by vertical surfaces
- Theoretical pressure distributions for some slender wing-body combinations at zero lift
- Wind-tunnel investigation of jet-augmented flaps on a rectangular wing to high momentum coefficients
- Altitude performance of J71-A-2(600-D1) turbojet engine
- Turbulent shear spectra and local isotropy in the low-speed boundary layer
- Aerodynamic and hydrodynamic characteristics of a deck-inlet multijet water-based-aircraft configuration designed for supersonic flight
- Additional results of an investigation at transonic speeds to determine the effects of a heated propulsive jet on the drag characteristics of a series of related afterbodies
- Theoretical wave drag of shrouded airfoils and bodies
- Two-dimensional low-speed cascade investigation of NACA compressor blade sections having a systematic variation in mean-line loading
- Use of a diffuser Mach number as a supersonic-inlet control parameter
- Low-speed measurements of static stability, damping in yaw, and damping in roll of a delta, a swept, and an unswept wing for angles of attack from 0 degrees to 90 degrees
- Low-speed pressure-distribution investigation of a spoiler and a spoiler-slot-deflector on a 30 degree sweptback wing-fuselage model having an aspect ratio of 3, a taper ratio of 0.5, and NACA 65A004 airfoil section
- Low-speed pressure-distribution investigation of a thin-delta-wing-fuselage model with double slotted flap, extended double slotted flap, and canard