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NACA Research Memorandums
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Preliminary Investigation at a Mach Number of 1.9 and a Reynolds Number of 2,200,000 of Three Ailerons Applicable to the Bell XS-2 Airplane Design
Wind-Tunnel Investigation of the Low-Speed Stability and Control Characteristics of a Model With a Sweptback Vee Tail and a Sweptback Wing
Effects of inlet icing on performance of axial-flow turbojet engine in natural icing conditions
Investigation of annular liquid flow with concurrent air flow in horizontal tubes
Limits of Flammability of Pure Hydrocarbon-Air Mixtures at Reduced Pressures and Room Temperature
Effect of rotor- and stator-blade modifications on surge performance of an 11-stage axial-flow compressor 2: redesigned compressor for XJ-40-WE-6 engine
Free-Jet Altitude Investigation of a 20-Inch Ram-Jet Combustor With a Rich Inner Zone of Combustion for Improved Low-Temperature-Ratio Operation
De-Icing and Runback Characteristics of Three Cyclic Electric, External De-Icing Boots Employing Chordwise Shedding
De-icing and runback characteristics of three cyclic electric, external de-icing boots employing chordwise shedding
Analysis of Factors Affecting Selection and Design of Air-Cooled Single-Stage Turbine for Turbojet Engines 1: Turbine Performance and Engine Weight-Flow Capacity
Experimental investigation of the effect of a shrouded rotor on the performance of a conservatively designed turbine
Investigation of a high-temperature single-stage turbine suitable for air cooling and turbine stator adjustment 1: design of vortex turbine and performance with stator at design setting
Photographic Study of Rotary Screaming and Other Oscillations in a Rocket Engine
The Effect of Wing Fences on the Longitudinal Characteristics at High Subsonic Speeds of a Wing-Fuselage-Tail Combination Having a Wing With 40 Degrees of Sweepback and NACA Four-Digit Thickness Distribution
The effect of wing height on the longitudinal characteristics at high subsonic speeds of a wing-fuselage-tail combination having a wing with 40 degrees of sweepback and NACA four digit thickness distribution
Effects of spanwise location of sweep discontinuity on the low-speed static lateral stability characteristics of a complete model with wings of M and W plan form
Experimental Static Aerodynamic Forces and Moments at Low Speed on a Missile Model During Simulated Launching From the 25-Percent-Semispan and Wing-Tip Location of a 45 Degree Sweptback Wing-Fuselage Combination
Flight measurements of wing loads on the Convair XF-92A delta-wing airplane
Low-Speed Investigation of the Effects of Wing Tanks and Speed Brakes on the Static Stability of a Model Having a 40 Degree Swept Wing
Analytic evaluation of effect of inlet-air temperature and combustion pressure on combustion performance of boron slurries and blends of pentaborane in octene-1 : Supplement I - Influence of new boric-oxide vapor-pressure data on calculated performanc
Effect of combustion-chamber pressure and nozzle expansion ratio on theoretical performance of several rocket propellant systems
A horizontal-tail arrangement for counteracting static longitudinal instability of sweptback wings
Preliminary investigation of short two-dimensional subsonic diffusers
A Summary of Results Obtained During Flight Simulation of Several Aircraft Prototypes With Variable-Stability Airplanes
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