Browse TRAIL Inventories

Lateral-control characteristics of North American XP-51 airplane (A. C. No. 41-38) with beveled trailing-edge ailerons in high-speed flight

A mass-distribution criterion for predicting the effect of control manipulation on the recovery from a spin

The Porpoising Characteristics of a Planing Surface Representing the Forebody of a Flying-Boat Hull

Power-on longitudinal-stability and control tests of the 1/8-scale model of the Brewster F2A airplane equipped with full-span slotted flaps and a new horizontal tail

Preliminary Investigation in the NACA Low-Turbulence Tunnel of Low-Drag Airfoil Sections Suitable for Admitting Air at the Leading Edge

The effect of pitch on force and moment characteristics of full-scale propellers of five solidities

The effect of spanwise mass distribution upon the spin characteristics of airplanes as determined by model tests conducted in the free-spinning wind tunnel

Wind-tunnel investigation of a tapered wing with a plug-type spoiler-slot aileron and full-span slotted flaps

Wind tunnel investigation of a plain aileron with various trailing-edge modifications on a tapered wing 2: ailerons with thickened and beveled trailing edges

Methods used in the NACA tank for the investigation of the longitudinal-stability characteristics of models of flying boats

Wind-tunnel investigation of a plain aileron and a balanced aileron on a tapered wing with full-span duplex flaps

Multiengine airplane spin characteristics as indicated by model tests in the free-spinning wind tunnel

Wind-Tunnel Investigation of Control-Surface Characteristics: [Part] 7 - A Medium Aerodynamic Balance of Two Nose Shapes Used With a 30-Percent-Chord Flap on an NACA 0015 Airfoil

Wind Tunnel Investigation of Effect of Yaw on Lateral-Stability Characteristics: [Part] 4 - Symmetrically Tapered Wing With a Circular Fuselage Having a Wedge-Shaped Rear and a Vertical Tail

Wind tunnel investigation of control surface characteristics 9: some analytical considerations and experimental test results for an internally balanced flap

Wind-tunnel investigation of control-surface characteristics 6: a 30-percent-chord plain flap on the NACA 0015 airfoil

Wind tunnel investigation of control-surface characteristics 10: a 30-percent-chord plain flap with straight contour on the NACA 0015 airfoil

The Photoviscous Properties of Fluids

The Electrical Structure of Thunderstorms

Annual Report of the National Advisory Committee for Aeronautics (27th). Administrative Report Including Technical Report Nos. 704 to 726

The Formation of Ice on Aircraft

The Icing of Aircraft

The Longitudinal Stability of Flying Boats as Determined by Tests of Models in the NACA Tank 2: Effect of Variations in Form of Hull on Longitudinal Stability

Cooling in Cruising Flight With Low Fuel-Air Ratios

Effects of Direction of Propeller Rotation on the Longitudinal Stability of the 1/10-Scale Model of the North American XB-28 Airplane With Flaps Neutral

Drag and Propulsive Characteristics of Air-Cooled Engine-Nacelle Installations for Large Airplane

The Effect of Cowling Shape on the Stability Characteristics of an Airplane

Recent Results in Rocket Flight Technique

The Effect of Solidity, Blade Section, and Contravane Angle on the Characteristics of an Axial-Flow Fan

Analysis of Heat and Compressibility Effects in Internal Flow Systems and High-Speed Tests of a Ram-Jet System

Cooling Tests of an Air-Cooled Engine Cylinder With Copper Fins on the Barrel

Contribution to the Design of Plywood Shells

Aerodynamics of the Fuselage

A Brief Study of the Speed Reduction of Overtaking Airplanes by Means of Air Brakes

Generalized Selection Charts for Harrison and Tubular Intercoolers

The Performance of a Vaneless Diffuser Fan

The Navier-Stokes Stress Principle for Viscous Fluids

Two-Dimensional Potential Flow Past an Ordinary Thick Wing Profile

Wind-Tunnel Investigations of Diving Brakes

Theory of Heat Transfer in Smooth and Rough Pipes

Application of Balancing Tabs to Ailerons

Aerodynamic Characteristics and Flap Loads of the Brake-Flap Installation on the 0.40-Scale Model of the F4F-3 Left Wing Panel

Adjustment of Stick Force by a Nonlinear Aileron-Stick Linkage

Aerodynamic Characteristics for Internal-Balance and Frise Type Ailerons on an NACA 6 Series Low-Drag Tip Section of the Wing for the XP-63 Airplane

The Aerodynamic Tests of Three Edo Floats for the SB2U-3, 0S2U-2, and XSB2C-2 Seaplanes - NACA Models 106-K, 107-K, and 125-AH

Aerodynamic Tests of an M-31 Bomb in the 8-Foot High-Speed Tunnel

Self-Ignition and Combustion of Gases

High-Speed Tests of a Model Twin-Engine Low-Wing Transport Airplane

High-Speed Wind-Tunnel Tests of Gun Openings in the Nose of the Fuselage of a 1/4-Scale Model

Flight Measurements of the Aileron Characteristics of a Grumman F4F-3 Airplane


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