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NACA Advanced Confidential Reports
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The development and application of high-critical-speed nose inlets
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
Experimental verification of a simplified vee-tail theory and analysis of available data on complete models with vee tails
Determination of the Effect of Horizontal-Tail Flexibility on Longitudinal Control Characteristics
Wind-tunnel tests of a blunt-nose aileron with beveled trailing edge on an NACA 66(215)-216 airfoil with several modifications of aileron nose and adjacent airfoil contour
Flight Investigation of Boundary-Layer Transition and Profile Drag of an Experimental Low-Drag Wing Installed on a Fighter-Type Airplane
Flight Tests of Dive-Recovery Flaps on an XP-51 Airplane
Wind-Tunnel Investigation of a High-Critical-Speed Fuselage Scoop Including the Effects of Boundary Layer
A flight investigation of NACA aileron modifications for the improvement of the lateral control characteristics of a high-speed fighter airplane
Comparison of fixed-stabilizer, adjustable- stabilizer and all-movable horizontal tails
Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil
Two-dimensional wind-tunnel investigation of 0.20-airfoil-chord plain ailerons of different contour on an NACA 65(sub 1)-210 airfoil section
Determination of the Stability and Control Characteristics of a Tailless All-Wing Airplane Model with Sweepback in the Langley Free-Flight Tunnel
Effect of Wing Modifications on the Longitudinal Stability of a Tailless All-Wing Airplane Model
A theoretical analysis of the performance of a diesel engine-compressor-turbine combination for aircraft
Knock-limited power outputs from a CFR engine using internal coolants 2: six aliphatic amines
An Electron-Diffraction Examination of Cast-Iron Piston Rings From Single-Cylinder Aircraft Engine Tests
An Electron and X-Ray Diffraction Investigation of Surface Changes on Nitrided-Steel Piston Rings During Engine Operation in Nitrided-Steel Cylinders Barrels
Effect of the Lift Coefficient on Propeller Flutter
Flight Investigation of Boundary-Layer and Profile-Drag Characteristics of Smooth Wing Sections of a P-47D Airplane
Flight Investigation of Boundary-Layer Transition and Profile Drag of an Experimental Low-Drag Wing Installed on a Figher-Type Airplane
Charts for Helicopter-Performance Estimation
Efficiency tests of a single-stage impulse turbine having an 11.0-inch pitch-line diameter wheel with air as the driving fluid
The Effect of Inlet Pressure and Temperature on the Efficiency of a Single Stage Impulse Turbine Having an 11.0-Inch Pitch-Line Diameter Wheel
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