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Experimental investigation of aerodynamically balanced trailing-edge control surfaces on an aspect ratio 2 triangular wing at subsonic and supersonic speeds
Comparison of Wind-Tunnel Predictions with Flight Measurements of the Longitudinal-Stability and -Control Characteristics of a Douglas BTD-1 Airplane
The Origin and Distribution of Supsonic Store Interference From Measurement of Individual Forces on Several Wing-Fuselage-Store Configurations 5 - Swept-Wing Heavy-Bomber Configuration With Large Store (Nacelle). Mach Number, 2.01
The Origin and Distribution of Supersonic Store Interference From Measurement of Individual Forces on Several Wing-Fuselage-Store Configurations 5: Swept-Wing Heavy-Bomber Configuration With Large Store (Nacelle). Mach Number 2.01
Permeability variation of a taper-rolled wire cloth
Spontaneous Flammability of Pentaborane and Pentaborane-3-Methylpentane Blends
Evaluation of Gust and Draft Velocities from Flights of F-61C Airplanes within Thunderstorms August 7, 1947 to August 13, 1947 at Clinton County Army Air Field, Ohio
Evaluation of Gust and Draft Velocities From Flights of P-61C Airplanes Within Thunderstorms July 31, 1947 to August 6, 1947 at Clinton County Army Air Field, Ohio
Analytical Investigation of Propeller Efficiency at High Subsonic Flight Speeds near Mach Number Unity
Theoretical analysis of the performance of a supersonic ducted rocket
Application of Tchebichef form of harmonic analysis to the calculation of zero-lift wave drag of wing-body-tail combinations
An Investigation at Mach Numbers 2.98 and 2.18 of Axially Symmetric Free-Jet Diffusion with a Ram-Jet Engine
Preliminary investigation of combustion of diborane in a turbojet combustor
Experiments on the distribution of fuel in fuel sprays
The Time Lag Between Flap Deflection and Force Development at a Mach Number of 4
Aerodynamic Characteristics at High Speeds of Full-Scale Propellers Having Different Shank Designs
Some Operating Experience and Problems Encountered During Operation of a Free-Jet Facility
Effects of Obstructions in Compressor Inlet on Blade Vibration in 10-Stage Axial-Flow Compressor
A study of a symmetrical, circular, internal, compression inlet
Aerodynamics of bodies, wings, and wing-body combinations at high angles of attack and supersonic speeds
Force, moment, and pressure-distribution characteristics of rectangular wings at high angles of attack and supersonic speeds
Analytical and experimental investigation of inlet-engine matching for turbojet-powered aircraft at Mach numbers up to 2.0
Effect of design changes and operating conditions on combustion and operational performance of a 28-inch diameter ram-jet engine
Effect of Design Changes of Operating Conditions on Combustion and Operational Performance of a 28-Inch Diameter Ram-Jet Engine
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