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NACA Wartime Reports
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NACA Wartime Reports
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The Knock-Limited Performance of S Reference Fuel Plus 2 Milliliters of Triethylthallium Per Gallon
Ditching Tests With 1/10-Size Model of the Army a-20a Airplane 1: Calm-Water Tests in NACA Tank No.2
On the Flow of a Compressible Fluid by the Hodography Method 2: Fundamental Set of Particular Flow Solutions of the Chaplygin Differential Equation
The effect of exhaust-stack shape on the design and performance of the individual cylinder exhaust-gas jet-propulsion system
The problem of longitudinal stability and control at high speeds
The Flow of a Compressible Fluid Past a Curved Surface
Secondary Stresses in Open Box Beams Subjected to Torsion
Flight Investigation at High Mach Numbers of Several Methods of Measuring Static Pressure on an Airplane Wing
Effects of Compressibility on the Maximum Lift Characteristics and Spanwise Load Distribution of a 12-Foot-Span Fighter-Type Wing of NACA 230-Series Airfoil Sections
Wind-Tunnel Investigation of Perforated Split Flaps for Use as Dive Brakes on a Tapered NACA 23012 Airfoil
Wind-Tunnel Development of a Plug-Type Spoiler-Slot Aileron for a Wing With a Full-Span Slotted Flap and a Discussion of Its Application
Critical shear stress of an infinitely long flat plate with equal elastic restraints against rotation along the parallel edges
Estimates of the Vertical-Tail Loads of a Bell P-63A-1 Airplane (AAF No. 42-68889) in Accelerated Rolling Maneuvers Based on Flight Tests With Two Vertical-Tail Arrangements
Adjustment of Stick Force by a Nonlinear Aileron-Stick Linkage
Wind-Tunnel Tests of a Piston-Type Control Booster on an Airfoil and Aileron Model
Tests of a 0.1475c Aileron With a Tab on Low-Drag Section for Curtiss XP-60 Airplane in the Low-Turbulence Tunnel
An Investigation of the Mutual Interference Effects of a Tail-Surface: Stern Propeller Installation on a Model Simulating the Douglas XB-42 Empennage
Lift and drag data for 30 pusher-propeller shaft housings on an NACA 65,3-018 airfoil section
Effects of Reynolds Number and Leading-Edge Roughness on Lift and Drag Characteristics of the NACA 653-418, a=1.0 Airfoil Section
Aerodynamic Tests of an NACA 66(215)-116, a=0.6 Airfoil With a 0.25c Slotted Flap for the Fleetwings XA-39 Airplane
Full-Scale Tunnel Investigation of the Control and Stability of a Twin-Engine Monoplane With Propellers Operating
Control-Motion Studies of the PBM-3 Flying Boat in Abrupt Pull-Ups
The Theory of Propellers 3: The Slipstream Contraction With Numerical Values for Two-Blade and Four-Blade Propeller
The Theory of Propellers 4: Thrust, Energy, and Efficiency Formulas for Single- and Dual-Rotating Propellers With Ideal Circulation Distribution
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