Browse TRAIL Inventories

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

Generalized equations for selection charts for heat exchangers in aircraft

Generalized selection charts for bombers powered by one, two, four, and six 3000-horsepower engines 1: capacity and economy

Generalized selection charts for bombers with four 2000-horsepower engines

High-Speed Tests of a Ducted Body with Various Air-Outlet Openings

Generalized selection charts for bombers powered by two, four, and six 3000-horsepower engines

Shear-lag tests of two box beams with flat covers loaded to destruction

Propeller Blade Stresses Caused by Periodic Displacement of the Propeller Shaft

Correlation of Data on the Statistical Theory of Turbulence

Free-spinning-tunnel tests of a 1/23.75-scale model of the Douglas DC-3 airplane

Effect of airplane design efficiency and engine economy on range

Flight tests of NACA jet-propulsion exhaust stacks on the supermarine spitfire airplane


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