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NACA Technical Notes
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The aerodynamic forces and moments on a 1/10-scale model of a fighter airplane in spinning attitudes as measured on a rotary balance in the Langley 20-foot free-spinning tunnel
Aerodynamic investigation of a parabolic body of revolution at Mach number of 1.92 and some effects of an annular supersonic jet exhausting from the base
Aerodynamics characteristics of 24 NACA 16-series airfoils at Mach numbers between 0.3 and 0.8
The Aileron as an Aid to Recovery From the Spin
Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow
Airfoil lift with changing angle of attack
Airfoil profiles for minimum pressure drag at supersonic velocities: Application of shock-expansion theory, including consideration of hypersonic range
Alterations and Tests of The "Farnboro" Engine Indicator
Analysis for Control Application of Dynamic Characteristics of Turbojet Engine With Tail-Pipe Burning
An analysis of acceleration, airspeed, and gust-velocity data from a four-engine transport airplane in operations on an eastern United States route
Analysis of Dr. Schaffran's Propeller Model Tests
Analysis of effect of variations in primary variables on time constant and turbine-inlet-temperature overshoot of turbojet engine
Analysis of Performance of a Jet Engine From Characteristics of Components 2: Interaction of Components as Determined From Engine Operation
Analysis of Pure-Bending Flutter of a Cantilever Swept Wing and Its Relation to Bending-Torsion Flutter
An Analysis of Ramjet Engines Using Supersonic Combustion
Analysis of shock motion in ducts during disturbances in downstream pressure
An analysis of the airspeeds and normal accelerations of Boeing S-307 airplanes in commercial transport operation
An analysis of the airspeeds and normal accelerations of Douglas DC-3 airplanes in commercial transport operation
An analysis of the airspeeds and normal accelerations of Martin M-130 airplanes in commercial transport operation
Analysis of the Creep Behavior of a Square Plate Loaded in Edge Compression
An analysis of the effect of lift-drag ratio and stalling speed on landing-flare characteristics
Analysis of the Horizontal-Tail Loads Measured in Flight on a Multiengine Jet Bomber
An Analysis of Turbojet-Engine-Inlet Matching
Analysis of Turbulent Flow and Heat Transfer in Noncircular Passages
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